Zusammenfassung
Die ersten beiden Abschnitte dieses Kapitels behandeln die Antriebsbahn (5.1) bzw. die Freiflugbahn (5.2), S. 356, von Geschoß und Rakete einschließlich des Problems des Wiedereintritts von irgendwelchen Flugkörpern, insbesondere von künstlichen Erdsatelliten, in die Erdatmosphäre (5.2.23), S. 369. Im folgenden Abschnitt 5.3, S. 372, wird die Keplerbewegung einbezogen und die Differentialgleichungen der Bahnelemente bei beliebigen Störungen auf anschaulichem Wege hergeleitet. Der Einfluß der Erdabplattung auf die Satellitenbahn (5.4), S. 396, die Lebensdauer eines Satelliten bei Berücksichtigung des Luftwiderstandes (5.5), S. 407, und der Übergang von einer Keplerbahn in eine andere mit Hilfe von Zusatzimpulsen (5.6), S. 413, sind im Grunde nur spezielle Anwendungen der Störungstheorie. Wegen der außerordentlich intensiven Bearbeitung, die diese drei Probleme in den letzten Jahren erfahren haben, ist jedoch ihrer Einführung jeweils ein besonderer Abschnitt vorbehalten.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
Preview
Unable to display preview. Download preview PDF.
Literatur zu Kap. V
a) Bücher
Bauschinger, J.: Die Bahnbestimmung der Himmelskörper. Leipzig, 1906.
Charbonnier, P.: Balistique intérieure. Paris, 1908.
Cranz, C.: Lehrbuch der Ballistik. Bd. I. Äußere Ballistik. Berlin, 1925. Bd. 2. Innere Ballistik. 1926.
Hohmann, W.: Die Erreichbarkeit der Himmelskörper. München, 1925.
Bollé, E.: Innere Ballistik. In F. Auerbach und W. Hort (Herausg.): Handbuch der physikalischen und technischen Mechanik. Bd. II, 1, S. 276–325. Leipzig, 1928.
Oberth, H.: Wege zur Raumschiffahrt. München, 1928.
Rosser, J. B. u. a.: Mathematical theory of rocket flight. New York, 1947.
Sänger, R.: Ballistische Störungstheorie unter besonderer Berücksichtigung der Wettereinflüsse. Basel, 1949.
N.N.: Oerlikon Taschenbuch, Zürich-Oerlikon, 1956. ( Artikel über innere und äußere Ballistik, Meßtechnik und Sonderwaffen).
Royal Aeronautical Society u. a.: High altitude and satellite rockets. (Symposium Cranfield, 1957). New York, 1959.
Stumpff, K.: Himmelsmechanik. Bd. I (1959), Bd. II. Berlin, 1965.
Stutz, W.: Schießlehre. Basel, 1959.
Berman, A. I.: The physical principles of astronautics. New York, 1961.
Brouwer, D. und G. M. Clemence: Methods of celestial mechanics. New York, 1961.
Ehricke, K A.: Space flight. I. Environment and celestial mechanics. II. Dynamics. III. Operations. New York, 1961.
Morrow, C. T. u. a. (Herausg.): Ballistic missile and space technology. New York, 1961.
Duncan, R. C.: Dynamics of atmospheric entry. New York, 1962.
Leitmann, G. (Herausg.): Optimization techniques. With application to aerospace systems. New York, 1962.
Moulton, F. R.: Methods in exterior ballistics. New York, 1962.
Nelson, W. C. und E. E. Loft: Space mechanics. Englewood Cliffs, N. J., 1962.
Roberson, R. E. und J. S. Farrior (Herausg.): Guidance and control. New York, 1962.
Salmon, M.: Principes du vol balistique et spatial. Paris, 1962.
Bohrmann, A.: Bahnen künstlicher Satelliten. Mannheim, 1963.
Brüning, G.: Flugmechanische Probleme an Raumfahrt- und Wiedereintrittsflugkörpern. 2. Lehrgang für Raumfahrttechnik (Braunschweig 1963) Bd. II, 301–1/153.
Lawden, D. F.: Optimal trajectories for space navigation. London, 1963.
Leondes, C. T. (Herausg.): Guidance and control of aerospace vehicles. New York, 1963.
Loh, W. H. T.: Dynamics and thermodynamics of planetary entry. Englewood Cliffs, N. J., 1963.
Petersen N. V. (Herausg.): Advances in astronautical sciences. Bd. 16, Teil I und II: Space rendezvous, rescues and recovery. New York, 1963.
Riley, F. E. und J. D. Sailor: Space systems engineering. New York, 1963.
Rössger, E. und H. Zehle: Grundlagen der Raumfahrzeugführung. Köln, 1963.
White, J. F. (Herausg.): Flight performance handbook for powered flight operations, flight mechanics and space vehicle design, empirical formula, analytic approximations and graphical aids. London, 1963.
Wolverton, R. W.: Flight performance handbook for orbital operations. New York, 1963.
Battin, R. H.: Astronautical guidance. New York, 1964.
Gantmakher, F. R. und L. M. Levin: The flight of uncontrolled rockets. Oxford, 1964.
King-Hele, D.: Theory of satellite orbits in an atmosphere. London, 1964.
Koelle, H. H.: Theorie und Technik der Raumfahrzeuge. Stuttgart, 1964.
Kurnosova, L. V. (Herausg.): Artificial earth satellites. Bd. 16. New York, 1964. ( Zahlreiche Artikel zum Rückkehr- bzw. Rendezvous-Problem).
Langford, R. C. und Ch. J. Mundo (Herausg.): Guidance and control II. New York, 1964.
Szebehely, V. G. (Herausg.): Celestial mechanics and astrodynamics. New York, 1964.
Groves, G. V. (Herausg.): Dynamics of rockets and satellites. Amsterdam, 1965.
Seigel, A. E.: The theory of high speed guns. AGARDograph 91 (Mai 1965 ).
Vertregt, M.: Principles of astronautics. New York, 1965.
Love, A. E. H. und F. R. Pidduck: Lagrange’s ballistic problem. Phil. Trans. Roy. Soc. A 222, 167–226 (1922).
Thornhill, C. K.: A new special solution to the complete problem of the internal ballistics of guns. AGARD Rep. 550 (1966).
Krause, H. G. L.: Allgemeine Theorie der Stufenraketen. Weltraumfahrt 4, 52–59 (1953).
Ehricke, K. A.: Ascent of orbital vehicles. Astronaut. Acta 2, 175–190 (1956).
Perkins, F. M.: Flight mechanics of ascending satellite vehicles. ARS Journal 26, 352–358 (1956).
Reece, J. W. u. a.: Ballistic missile performance. ARS Journal 26, 251–255 (1956).
West, C. D.: Boost phase trajectory analysis techniques. ARS Journal 27, 527–533 (1957).
Koelle, H. H.: Über eine Näherungsmethode zur Berechnung von Kreisbahnraketen. Raketentechnik und Raumfahrtforschung 2, 8–12 (1958).
Koelle, H. H.: On the development of orbital techniques. IX. Kongr. Internat. Astronaut. Amsterdam, 1958, Bd. II, S. 702–746.
Scholze, O.: Einflußgrößen ballistischer Fern-Flugkörper. Raketentechnik und Raumfahrtforschung 2, 2–8 (1958).
Singer, S. F. und R. C. Wentworth: A method for calculating impact points of ballistic rockets. ARS Journal 27, 407–409 (1957) und 28, 684–687 (1958).
Struble, R. A. u. a.: The trajectory of a rocket with thrust. ARS Journal 28, 472–478 (1958).
Veubeke, Fraeijs de, B.: Le problème du maximum de rayon d’action dans un champ de gravitation uniforme. Astronaut. Acta 4, 1–14 (1958).
Weisbord, L.: A generalized optimization procedure for N-staged missiles. ARS Journal 28, 164–167 (1958).
Froehlich, J. E. und A. R. Hibbs: Ballistics of the Explorer. In: W. C. Nelson (Herausg.): Selected topics on ballistics, S. 59–73. AGARD. New York, 1959.
Hoelker, R. F.: Launching of Explorer I. In: W. C. Nelson (Herausg.): Selected topics on ballistics, S. 74–87. AGARD. New York, 1959.
Kelley, A. J.: Effect of thrust termination process upon range dispersion of a ballistic missile. ARS Journal 29, 432–440 (1959).
Scholze, O.: Graphische Ermittlung der Haupteinfluß- und Vorentwurfsgrößen von Flugkörpern. Raketentechnik und Raumfahrtforschung 3, 36–44 (1959).
Traenkle, C. A.: Mechanics of the power and launching phase for missiles and satellites. Ing. Archiv 28, 335–356 (1959).
Chase, R. L.: Multistage rocket staging optimization. Adv. in Astronaut. Sci., Bd. 6, S. 621–629 (1960).
Froehlich, J. E.: Capabilities of multistaged chemical rocket systems. Astronaut. Acta 6, 311–321 (1960).
Koelle, H. H.: On the optimum size of orbital carrier vehicles based on overall economy. IX. Kongr. Internat. Astronaut. Stockholm, 1960, Bd. I, S. 365–376.
Kulakowski, L. J. und R. T. Stancil: Rocket boost trajectories for maximum burnout velocity. ARS Journal 30, 612–623 (1960).
Molitz, H.: Der Einfluß des Abkippeffekts auf die Schußweite von Raketen. Wehrtech. Monatshefte 57, 410–419 (1960).
Stümke, H.: Flugleistungsberechnung unbemannter Raketen. In: K. Schütte und H. K. Kaiser (Herausg.): Handbuch der Astronautik, Bd. I, S. 80–109. Konstanz, 1960.
Ehlers, F. E.: Missile trajectories with linear time variation of the sine or tangent of the thrust angle. ARS Journal 31, 631–636 (1961).
Schulz, W.: Ein Beitrag zur Theorie der Stufenraketen. Z. Flugwiss. 9, 394 401 (1961).
Thackwell, H. L. jr. und J. A. Vandenkerkhove: Optimum staging of solidpropellant rocket vehicles. Astronaut. Acta 7, 190–202 (1961).
Veubeke, Fraeijs de, B. M.: L’étagement optimum des groupes de fusées en fonctionnement parallèle. Astronaut. Acta 7, 359–375 (1961).
Cooper, R. S.: Performance of optimized multistage rockets. J. Aero. Sci. 29, 1339–1343 (1962).
Pollak, R. J.: Rapid determination of the interactions between the ballistic rocket and its trajectory. ARS Journal 32, 42–51 (1962).
Fan, L.-T. und C. Wan: Weight minimization of a step rocket by the discrete maximum principle. J. Spacecraft 1, 123–125 (1964).
Kiessling, W.: Einfluß spezieller Bedingungen beim Aufstieg auf die Auslegungsdaten einer Höhenforschungsrakete. Jahrbuch 1964 der WGLR, S. 245–252.
Koelle, D. E.: Zur Definition und Größe der Nutzlast bei Raumtransporter-Projekten. Raumfahrtforschung 8, 155–160 (1964).
Thomae, H. F.: A technique for optimization of ascent trajectories and propellant loadings of multistage space vehicles. Raumfahrtforschung 8, 115–123 (1964).
Cavoti, C. R.: Optimization of multistage processes. J. Spacecraft 2, 94–97 (1965).
Gray, J. S. and R. V. Alexander: Cost and weight optimization for multistage rockets. J. Spacecraft 2, 80–86 (1965).
Zee, C.-H.: Powered flight trajectories of rockets under constant tangential thrust. J. Astronaut. Sci. 12, 1–6 (1965).
Lawden, D. F.: Minimal trajectories. J. Brit. Interplanet. Soc. 9, 179–186 (1950).
Lawden, D. F.: Optimal programming of rocket thrust direction. Astronaut. Acta 1, 41–56 (1955).
Lawden, D. F.: Optimum launching of a rocket into an orbit about the earth. Astronaut. Acta 1, 185–190 (1955).
Fried, B. D. und J. M. Richardson: Optimum rocket trajectories. J. Appl. Phys. 27, 955–961 (1956).
Miele, A.: Optimum burning program as related to aerodynamic heating for a missile traversing the earth’s atmosphere. ARS Journal 27, 1231–1240 (1957).
Bryson, A. E. und S. E. Ross: Optimum rocket trajectories with aerodynamic drag. ARS Journal 28, 465–469 (1958).
Leitmann, G.: Optimum thrust direction for maximum range. J. Brit. Inter-planet. Soc. 16, 503–507 (1958).
Miele, A.: On the brachistochronic thrust program for a rocket-powered missile travelling in an isothermal medium. ARS Journal 28, 675–684 (1958).
Miele, A.: General variational theory of the flight paths of rocket-powered aircraft, missiles and satellite carriers. IX. Kongr. Internat. Astronaut. Amsterdam, 1958, Bd. II, S. 946–970 und Astronaut. Acta 4, 264–288 (1958).
Miele, A. und C. R. Cavoti: Optimum thrust programming along arbitrarily inclined rectilinear paths. Astronaut. Acta 4, 167–181 (1958).
Miele, A. und C. R. Cavoti: Generalized variational approach to the optimum thrust programming for the vertical flight of a rocket. Z. Flugwiss. 6, 69–77 und 102–109 (1958).
Newton, R. R.: On the optimum trajectory of a rocket. J. Franklin Inst. 266, 155–187 ( 1958 I I ).
Okhotsimskii, D. E. und T. M. Eneev: Some variation problems connected with the launching of artificial satellites of the earth. J. Brit. Interplanet. Soc. 16, 263–294 (1958).
Leitmann, G.: On a class of variational problems in rocket flight. J. Aero. Sci. 26, 586–591 (1959).
Miele, A. und J. O. Capellari jr.: Dynamic programming for rockets. Z. Flugwiss. 7, 14–21 (1959).
Traenkle, C. A.: Design parameters and optimization of missile trajectories. Z. Flugwiss. 7, 287–293 (1959).
Faulkner, F. D.: Complete elementary solution to some optimum trajectory problem. ARS Journal 31, 33–39 (1961).
Leitmann, G.: An elementary derivation of the optimal control conditions. XII. Kongr. Internat. Astronaut. Washington, D. C., 1961, Bd. I, S. 275–298.
Miele, A.: The relation between the Green’s theorem approach and the direct methods for extremal problems of a linear type. XII. Kongr. Internat. Astronaut. Washington, D. C., 1961, Bd. I, S. 317–334.
Stancil, R. T. und L. J. Kulakowski: Rocket boost vehicle missions optimization. ARS Journal 31, 935–943 (1961).
Contensou, P.: Etude théorique des trajectoires optimales dans un champ de gravitation. Astronaut. Acta 8, 134–150 (1962).
Leitmann, G.: The optimization of rocket trajectoires — A survey. In: Progress in the Astronautical Sciences. Bd. I, S. 145–213. Amsterdam, 1962.
Schnäbele, W.: Raketen- und Bahnoptimierung. WGL-Lehrgang für Raumfahrttechnik (München 1962), Bd. II, 18–1/21.
Lawden, D. F.: Analytical techniques for the optimization of rocket trajectories. Aeronaut. Quart. 14, 105–124 (1963).
Lutz, O. (Herausg.): 2. Lehrgang für Raumfahrttechnik ( Braunschweig 1963 ), Bd. I. Mehrere Beiträge zur Frage der Bahnoptimierung.
Denham, W. F.: Range maximization of a surface-to-surface missile with in-flight inequality constreints. J. Spacecraft 1, 78–83 (1964).
Heermann, H. und Ph. Kretsinger: The minimum time problem. J. Astronaut. Sci. 11, 93–107 (1964).
Keller, J. L.: On minimum propellant paths for thrust limited rockets. Astronaut. Acta 10, 262–269 (1964).
Kelley, H. J.: A second variation test for singular extremals. AIAA Journal 2, 1380–1382 (1964).
Lawden, D. F.: Trajectory optimization for a rocket with a generalized thrust characteristic. Astronaut. Acta 10, 279–295 (1964).
Pines, S.: Constants of the motion for optimum thrust trajectories in a central force field. AIAA Journal 2, 2010–2014 (1964).
Rosenbloom, A.: Application of optimization techniques. AGARDograph 92 (Okt. 1964 ), S. 1–21.
Schulz, W. und H.-K. Schulze: Die Methode des Dynamic Programming und ihre Anwendung auf Optimierungsaufgaben der Flugmechanik. Jahrbuch 1964 der WGLR, S. 238–244.
Standl, R. T.: A new approach to steepest-ascent trajectory optimization. AIAA Journal 2, 1365–1370 (1964).
Bell, D. J.: Optimal trajectories and the accessory minimum problem. Aeronaut. Quart. 16, 205–220 (1965).
Halkin, H.: Optimal aerodynamic steering for anti-ICBM missiles. J. Astronaut. Sci. 12, 71–82 (1965).
Kopp, R. E. und H. G. Moyer: Necessary conditions for singular extremals. AIAA Journal 3, 1439–1444 (1965).
Mason, J. D. u. a.: A variational method for optimal staging. AIAA Journal 3, 2007–2012 (1965).
Munick, H.: Goddard problem with bounded thrust. AIAA Journal 3, 1283–1285 (1965).
Narjes, O.: Über die Bestimmung optimaler, singulärer Steuerungen mit Hilfe des Maximumsprinzips von Pontrjagin. Z. Flugwiss. 13, 252–254 (1965).
Fasella, E.: Tavole balistiche secondarie. Genua, 1901 (zitiert nach H. Athen [6–001]).
Slacci, F.: Sur un problème d’Alembert. Compt. Rend. Ac. Sci. 132, 11751178 und 133, 381–382 (1901).
v. Eberhard, O.: Benutzung der Fasella-Tabellen zur stufenweisen Flugbahnberechnung unter Berücksichtigung der neuen Versuche über den Luftwiderstand ZAMM 11, 253–273 (1931).
Eckel, K.: Die ballistische Störungstheorie. Wehrtech. Monatshefte 52, 10–19, 45–51, 80–84 (1955).
Molitz, H.: Der Einfluß eines konstanten Windes auf die Bahn von Geschossen und Raketen. Wehrtech. Monatshefte 57, 258–268 (1960).
Schweikert, E.: Ballistischer Rechenschieber zur Bestimmung von Geschwindigkeiten und Flugzeiten für Flachbahnen. Wehrtech. Monatshefte 57, 467–475 (1960).
Curti, P.: Zur Graphik der Geschoßbahn. Wehrtech. Monatshefte 57, 334–349, 375–380 (1960), 58, 6–12 (1961), 60, 311–318, (1963).
Sanger, E. und I. Bredt: Ein Raketenantrieb für Langstreckenbomber. Dt. Luftfahrtforschung, UM 3538, 1944.
Stümke, H.: Zwei Flugbahnen des Gleiters A4b mit berichtigten Betriebsdaten (Beitrag zur Frage der zweckmäßigsten Flugart). Bericht Nr. 68/68 der Herresversuchsanstalt Peenemünde (1944).
Krause, H. G. L.: Strenge Integration der Bewegungsgleichung einer senkrecht aufsteigenden Rakete nach Brennschluß in der Atmosphäre. IV. Kongr. Internat. Astronaut. Zürich, 1953, S. 171–180.
Kaeppeler, H. J. und M. E. Kuebler: Die Rückkehr von geflügelten Geräten von Außenstations-Bahnen. V. Kongr. Internat. Astronaut. Innsbruck, 1954, S. 120–149.
Ehricke, K. A.: On the descent of winged orbital vehicles. Astronaut. Acta 1, 137–155 (1955).
Kaeppeler, H. J.: Über eine simultane analytische Integration der Bewegungsgleichungen eines geflügelten Gerätes im Überschallgleitflug. Astronaut. Acta 1, 166–170 (1955).
King-Hele, D. G.: The descent of an earth-satellite through the upper atmosphere. J. Brit. Interplanet. Soc. 15, 314–323 (1956).
Ferri, A. u. a.: The use of lift for re-entry from satellite trajectories. ARS Journal 27, 1184–1191 (1957).
Allen, H. J.: Hypersonic flight and the re-entry problem. J. Aero. Sci. 25, 217–227 (1958).
Allen, H. J. und A. J. Eggers jr.: A study of the motion and aerodynamic heating of ballistic missiles entering the earth’s atmosphere at high supersonic speeds. NACA Rep. 1381 (1958).
Baker, R. M. L. jr.: Enke’s method and variation of parameters as applied to re-entry trajectories. Adv. in Astronaut. Sci., Bd. 3, S. 36/1–10 (1958).
Bull, G. V. u. a.: Exit and re-entry problems. Aero/Space Eng. 17, 57–62 (Juni, 1958 ).
Eggers, A. J.: A comparative analysis of the performance of long-range hypervelocity vehicles. NACA Rep. 1382 (1958).
Roberson, R. E.: Oblateness correction to impact points of ballistic rockets. J. Franklin Inst. 266, 465–481 ( 1958 I I ).
Robinson, A. C. und A. J. Besonis: On the problems of re-entry into the earth’s atmosphere. Adv. in Astronaut. Sci., Bd. 3, S. 33/1–24 (1958).
Rosenberg, R. M.: On flight trajectories in the neighborhood of a known trajectory. J. Franklin Inst. 266, 109–128, ( 1958 I I ).
Allen, H. J.: Some aerodynamic effects on long-range rocket craft. In: W. C. Nelsen (Herausg.): Selected topics on ballistics, S. 46–58. AGARD. New York, 1959.
Chapman, D. R.: An approximate analytical method for studying entry into planetary atmospheres. NASA Tech. Rep. R-11 (1959).
Lees, L. u. a.: Use of aerodynamic lift during entry into the earth’s atmosphere. ARS Journal 29, 633–641 (1959).
Nonweiler, T.: The motion of an earth satellite on re-entry to the atmosphere. IX. Kongr. Internat. Astronaut. Amsterdam, 1958, Bd. II, 5.842–864. Astronaut. Acta 5, 40–62 (1959).
Paige, H. W.: The technology of manned return from outer space. J. Franklin Inst. 267, 103–118 ( 1959 I ).
Wheelon, A. D.: Free flight of a ballistic missile. ARS Journal 29, 915–926 (1959).
Chapman, D. R.: An analysis of the corridor and guidance requirements for supercircular entry into planetary atmospheres. NASA Tech. Rep. R-55 (1960) und X. Kongr. Internat. Astronaut. London, 1959, Bd. I, S. 254–267.
Loh, W. H. T.: Dynamics and thermodynamics of re-entry. J. Aero. Sci. 27, 748–762 (1960).
Loh, W. H. T.: Minor circle flight for boost glide or orbital reentry vehicles. Adv. in Astronaut. Sci. Bd. 6, S. 536–555 (1960).
Becker, J. V. u. a.: Aerodynamics of trajectory control for reentry at escape speed. Astronaut. Acta 7, 334–358 (1961).
Berman, L. J.: Optimum soft landing trajectories. XII. Kongr. Internat. Astronaut. Washington, D. C., 1961, Bd. I, S. 353–367.
Broglio, L.: Lois de similitude dans le calcul des trajectoires de rentrée et de l’ablation frontale des engins. Astronaut. Acta 7, 21–34 (1961).
Brun, E. A.: Considérations générales sur le problème de la rentrée. In: L. Broglio (Herausg.): Current Research in Astronaut. Sci., S. 296–321. New York, 1961.
Eggers, A. J. jr. und T. J. Wong: Motion and heating of lifting vehicles during atmosphere entry. ARS Journal 31, 1364–1375 (1961).
Loh, W. H. T.: A unified analytical solution for entry mechanics. XII. Kongr. Internat. Astronaut. Washington, D. C., 1961, Bd. I, S. 337–352.
Maday, C. J.: Aerodynamic capture of a ballistic type vehicle travelling at hyperbolic speed. XII. Kongr. Internat. Astronaut. Washington, D. C., 1961, Bd. I, S. 380–391.
Warden, R. V.: Ballistic re-entries with a varying W/cD A. ARS Journal 31, 208–213 (1961).
Wong, T. J. und R. E. Slye: The effect of lift on entry corridor depth and guidance requirements for the return lunar flight. NASA Tech. Rep. R-80 (1961).
Bate, R. R. und R. W. Johnson: Empirical formulas for ballistic re-entry trajectories. ARS Journal 32, 1882–1887 (1962).
Blum, R.: Re-entry trajectories: Flat earth approximation. ARS Journal 32, 616–620 (1962).
Broglio, L.: On guidance and landing accuracy requirements in re-entry trajectories. Astronaut. Acta 8, 245–263 (1962).
Bryson, A. E. u. a.: Determination of lift or drag programs to minimize re-entry heating. J. Aero. Sci. 29, 420–430 (1962).
Ferri, A. und Lu Ting: Practical aspects of re-entry problems. Astronaut. Acta 8, 63–81 (1962).
Hunziker, R. R.: Re-entry trajectories for impact prediction and radar acquisition. ARS Journal 32, 1261–1268 (1962).
Levinsky, E. S.: Application of inequality constreints to varational problems of lifting re-entry. J. Aero. Sci. 29, 400–409 (1962).
Loh, W. H. T.: Ballistic re-entry at small angles of inclination. ARS Journal 32, 718–721 (1962).
Loh, W. H. T.: A second-order theory of entry mechanics into a planetary atmosphere. J. Aero. Sci. 29, 1210–1221, 1237 (1962).
Mandell, D. S.: Maneuvring performance of lifting re-entry vehicles. ARS Journal 32, 346–354 (1962).
Moulin, L.: Précisions réquises pour les trajectoires de retour d’engins spatiaux. XIII. Kongr. Internat. Astronaut. Varna, 1962, Bd. II, S. 523–554.
Tempelman, W. H.: Selected problems in optimum ballistic descent from orbit. Astronaut. Acta 8, 193–204 (1962).
Wang, K. und Lu Ting: Approximate solutions for re-entry trajectories with aerodynamic forces. Astronaut. Acta 8, 28–41 (1962).
Elms, R. V. jr.: Projectile range in excess of 180°. AIAA Journal 1, 2406–2408 (1963).
Grant, F. C.: A theory of space probe entry under conditions of high mass loss. NASA TR 162 (1963).
Hoppe, H.: Flugbahnen für Wiedereintrittskörper mit Auftriebsvermögen. 2. Lehrgang für Raumfahrttechnik (Braunschweig 1963) Bd. II, 302–1/28.
Loh, W. H. T.: Some exact analytical solutions of planetary entry. AIAA Journal 1, 836–842 (1963).
Shen, Y. C.: Series solution of equations for re-entry vehicles with variable lift and drag coefficients. AIAA Journal 1, 2487–2490 (1963).
Wang, H. E. und S. T. Chu: Variable-lift re-entry at superorbital and orbital speeds. AIAA Journal 1, 1047–1055 (1963).
Wingrove, R. C.: Survey of atmosphere re-entry guidance and control methods. AIAA Journal 1, 2019–2029 (1963) und NASA Tech. Rep. R. 151 (1963).
Broglio, L.: A general theory on space and re-entry trajectories. AIAA Journal 2, 1774–1781 (1964).
Brunn, W.: Abstiegsbahnen für Raumflugkörper aus einer erdnahen Umlaufbahn. Jahrbuch 1964 der WGLR, S. 253–262.
Overesch, W.: Untersuchungen zum Problem des Wiedereintritts von Raumflugkörpern mit aerodynamischem Auftrieb. Jahrbuch 1964 der WGLR, S. 263–271.
Citron, S. J. und T. C. Meir: An analytic solution for entry into planetary atmospheres. AIAA Journal 3, 470–475 (1965).
Loh, W. H. T.: Extension of second-order theory of entry mechanics to oscillatory solutions. AIAA Journal 3, 1688–1691 (1965).
Smith, R. L.: Dynamics of an unusual spinning re-entry body. J. Spacecraft 2, 895–901 (1965).
Spielberg, I. N. und C. B. Cohen: Janus: a manned orbital spacecraft with staged re-entry. J. Spacecraft 2, 531–536 (1965).
Wang, H. E.: Motion of re-entry vehicles during constant-altitude glide. AIAA Journal 3, 1346–1348 (1965).
Spitzer, L. jr.: Perturbations of a satellite orbit. J. Brit. Interplanet. Soc. 9, 131–136 (1950).
Krause, H. G. L.: Die Säkularstörungen einer Außenstationsbahn. III. Kongr. Internat. Astronaut. Stuttgart, 1952, S. 162–173.
Schütte, K.: Die Bahnbestimmung aus dem Vektor der Bahngeschwindigkeit und der Einfluß einer Änderung desselben auf die Bahnelemente. IV. Kongr. Internat. Astronaut. Zürich, 1953, S. 89–102 und Weltraumfahrt 4, 98–107 (1953), 5, 13–20 (1954).
Krause, H. G. L.: Die säkularen und periodischen Störungen der Bahn eines künstlichen Erdsatelliten. VII. Kongr. Internat. Astronaut. Rom, 1956, S. 523–585.
Kooy, J. M. J.: On the application of the method of variation of elliptic orbit elements in case of a satellite vehicle. Astronaut. Acta 3, 179–214 (1957) und VII. Kongr. Internat. Astronaut. Rom, 1956, S. 705–739.
Roberson, R. E.: Orbital behavior of earth satellites. J. Franklin Inst. 264, 181–201, 269–285 ( 1957 I I ).
Gedeon, G. S.: Orbital mechanics of satellites. Adv. in Astronaut. Sci., Bd. 3, S. 19/1–33 (1958).
Herrick, S. und R. M. L. Baker jr.: Recent advances in astrodynamics. ARS Journal 28, 649–654 (1958).
King-Hele, I. G. und R. H. Merson: Satellite orbits in theory and practice. J. Brit. Interplanet. Soc. 16, 446–471 (1958).
Perkins, F. M.: An analytic solution for flight time of satellites in eccentric and circular orbits. Astronaut. Acta 4, 113–134 (1958).
Vertregt, M.: Die Bahnbestimmung aus dem Vektor der Bahngeschwindigkeit. Astronaut. Acta 4, 135–137 (1958).
Gedeon, G. S.: Kinematics of orbital motion. Adv. in Astronaut. Sci., Bd. 7, S. 87–98 (1960).
Gröbner, W. und F. Cap: Perturbation theory of celestial mechanics using Lie series. XI. Kongr. Internat. Astronaut. Stockholm, 1960, S. 348–350.
Herrick, S.: Observation requirement for precision orbit determination. In: N. J. Hopf und W. G. Vincenti (Herausg.): Aeronautics and Astronautics, Proc. Durand Centennial Conf., S. 417–434. New York, 1960.
Lanzano, P.: Application of lunar theory to the motion of satellite. Adv. in Astronaut. Sci., Bd. 6, S. 507–523 (1960).
Weirauch, R. F.: On the accuracy of an elliptic orbit determination. IX. Kongr. Internat. Astronaut. Stockholm, 1960, Bd. I, S. 377–384.
Kislik, M. D.: The motion of an artificial satellite in the normal gravitational field of the earth. Artificial Earth Satellites 4, 183–201 (1961).
Lur’e, A. I.: Equations of disturbed motion in the Kepler problem. Artificial Earth Satellites 4, 288–291 (1961).
Spiess, O. R.: Two notes in orbit theory. XII. Kongr. Internat. Astronaut. Washington, D. C., 1961, Bd. I, S. 121–130.
Arcese, A.: The importance of independent estimators in predicting orbital elements. J. Aero. Sci. 29, 1001–1002 (1962).
Dierstein, R.: Bahnen im Schwerefeld. WGL-Lehrgang für Raumfahrttechnik (München 1962) Bd. II,15–1/24.
Mitǎ, M. M.: Sur la possibilité de réalisation d’un vaisseau orbital stationnaire au-dessus d’un point non situé sur l’équateur terrestre. XIII. Kongr. Internat. Astronaut. Varna, 1962, Bd. II, S. 555–570.
Schmidt, W.: Bahnstörungen. WGL-Lehrgang für Raumfahrttechnik (München 1962) Bd. II, 17–1/18.
Thelan, H. T.: Computation of satellite orbits by the Hansen method as modified by Musen. NASA TR 147 (1962).
Traenkle, C. A.: Generalization and applications of the Keplerian time equation. Z. Flugwiss. 10, 306–314 (1962).
Wen, Li Shu: Differential expressions for nearly rectilinear and rectilinear closed orbits. J. Aero. Sci. 29, 1102–1104 (1962).
Wen, Li Shu: A unified treatment of „variation of parameters“and „differential expressions“methods in trajectory prediction and error analysis. J. Aero. Sci. 29, 61–66, 120 (1962).
Wong, P.: Nonsingular variation of parameter equations for computation of space trajectories. ARS Journal 32, 264–265 (1962).
El’yasberg, P. E.: Determination of orbits from two positions. Artificial Earth Satellites 13, 3–24 (1963).
Haviland, R. P. und C. M. House: Nonequatorial launching to equatorial orbits and general nonplanar launching. AIAA Journal 1, 1336–1342 (1963).
Kislik, M. D.: An analysis of the integrals of the equations of motion of an artificial satellite in the normal gravitational field of the earth. Artificial Earth Satellites 13, 25–55 (1963).
Lidov, M. L.: Evolution of the orbits of artificial satellites of planets as effected by gravitational perturbation from external bodies. AIAA Journal 1, 1985–2002 (1963).
Beckwith, R. E.: Approximate distribution of nearly circular orbits. AIAA Journal 2, 913–916 (1964).
Bell, P. 0.: Orbit determination by angular measurements. AIAA Journal 2, 1862–1864 (1964).
Chebotarew, G. A.: Motion of an artificial earth satellite in an orbit of small eccentricity. AIAA Journal 2, 203–208 (1964).
Danby, J. M. A.: Matrix methods in the calculation and analysis of orbits. AIAA Journal 2, 13–16 (1964).
Danby, J. M. A.: The matrizant of Keplerian motion. AIAA Journal 2, 16–19 (1964).
Lubowe, A. G.: High accuracy orbit prediction from node to node Astronaut. Acta 10, 253–261 (1964).
Nigam, R. C.: Orbital aspects of deployment of satellites. J. Astronaut. Sci. 11, 37–45 (1964).
Schröter, W.: Über die Bahnvoraussage von Erdsatelliten. Raumfahrtforschung 8, 10–16 (1964).
Lorell, J.: Long term behavior of artificial satellite orbits due to third-body perturbations. J. Astronaut. Sci. 12, 142–149 (1965).
Musen, P.: On the high order effects in the methods of Krylov-Bogoliubov and Poincaré. J. Astronaut. Sci. 12, 129–134 (1965).
Blitzer, L. u. a.: Perturbations of a satellite’s orbit due to the earth’s oblateness. J. Appl. Phys. 27, 1141–1149 (1956) und 28, 279, 1362 (1957).
Allen, W. A.: Effect on a rocket of the oblateness of a planet. ARS Journal 30, 623–627 (1960).
Anthony, M. L. u. a.: Escape from an oblate planet. Adv. in Astronaut. Sci., Bd. 7, S. 175–194 (1960).
Geyling, F. T.: Satellite perturbations from extraterrestrial gravitation and radiation pressure. J. Franklin Inst. 269, 375–407 ( 1960 I ).
Hall, N. S. und H. F. Gawlowicz: The oblatory perturbations of satellite orbits. Adv. in Astronaut. Sci., Bd. 6, S. 415–446 (1960).
Petty, C. M. und J. V. Breakwell: Satellite orbits about a planet with rotational symmetry. J. Franklin Inst. 270, 259–282 ( 1960 I I ).
Anthony, M. L. und G. E. Fosdick: Satellite motions about an oblate planet. J. Aero. Sci. 28, 789–802 (1961) und ARS Journal 31, 1225–1232 (1961).
King-Hele, D. G.: The effect of atmospheric oblateness on a satellite orbit. Astronaut. Acta 7, 390–405 (1961).
Mersman, W. A.: Theory of the secular variations in the orbit of a satellite of an oblate planet. NASA Tech. Rep. R-99 (1961).
Michielsen, H. F.: The effects of earth’s sectorial harmonics on a stationary satellite. XII. Kongr. Internat. Astronaut. Washington, D. C., 1961, Bd. I, S. 216–227.
Moc, M. M. und E. E. Karp: Effect of earth oblateness on the anomalistic period of a satellite. ARS Journal 31, 1462–1464 (1961).
Proskurin, V. F. und Y. V. Batrakov: Perturbations of the first order in the motion of artificial satellites, caused by flattening of the earth. Artificial Earth Satellites 3, 46–55 (1961).
Sarychew, V. A.: Influence of the flattening of the earth on the motion of an artificial earth satellite. Artificial Earth Satellites 6, 1–9 (1961).
Blitzer, L.: Synchronous and resonant satellite orbits associated with equatorial ellipticity. ARS Journal 32, 1016–1019 (1962).
Blitzer, L.: Circular orbits in an axially symmetric gravitational field. ARS Journal 32, 1102 (1962).
Brenner, J. L.: The equatorial orbit of a near earth satellite. ARS Journal 32, 1560–1563 (1962).
Frick, R. H. und T. B. Garber: Perturbations of a synchronous satellite due to triaxiality of the earth. J. Aero. Sci. 29, 1105–1111, 1114 (1962).
Lee, V. A.: Atmosphere oblateness correction factor for circular satellite orbits. ARS Journal 32, 102–103 (1962).
Lorell, J. und J. Anderson: Precession rates for an artificial satellite. XIII. Kongr. Internat. Astronaut. Varna, 1962, Bd. I, S. 451–461.
Mersman, W. A.: The critical inclination problem in satellite orbit theory. NASA Tech. Rep. R-148 (1962).
Sauer, C. G. jr.: Perturbations of a hyperbolic orbit by an oblate planet. ARS Journal 32, 714–717 (1962).
Sturms, F. M. jr.: Nodal period for a circular earth satellite. ARS Journal 32, 1037–1039 (1962).
Vries, de, J. P.: The sun’s perturbing effect on motion near a triangular Lagrange point. XIII. Kongr. Internat. Astronaut. Varna, 1962, Bd. I, S. 432–450.
Beletzkii, V. V.: Orbit of an equatorial earth satellite. Artificial Earth Satellites 13, 56–64 (1963).
Claus, A. J. und A. G. Lubowe: A high accuracy perturbation method with direct application to communication satellite orbit prediction. Astronaut. Acta 9, 275–301 (1963).
Escobal, P. R.: Rise and set time of a satellite about an oblate planet. AIAA Journal 1, 2306–2310 (1963).
Kalil, F.: Minimum altitude variation orbits about an oblate planet. AIAA Journal 1, 1655–1657 (1963).
Kalil, F. und F. Martikan: Derivation of nodal period of an earth satellite and comparisons of several first-order secular oblateness results. AIAA Journal 1, 2041–2046 (1963).
Perkins, F. M.: Flight mechanics of the 24-hour satellite. AIAA Journal 1, 848–851 (1963).
Geyling, F. T.: Closed-form coordinate perturbations of elliptical orbits due to oblateness. Astronaut. Acta 11, 196–201 (1965).
Lubowe, A. G.: Application of Lagrange’s planetary equations to orbits with low eccentricities, or low inclination, or both. J. Astronaut. Sci. 12, 7–17 (1965).
Petersen, N. V.: Lifetimes of satellites in near-circular and elliptic orbits. ARS Journal 26, 341–351, 368 (1956) und VII. Kongr. Internat. Astronaut. Rom, 1956, S. 789–810.
Henry, I. G.: Lifetimes of artificial satellites of the earth. ARS Journal 27, 21–24 (1957).
Casei, C. und V. Giavoto: Sul tempo di vita dei satelliti artificiali, IX. Kongr. Internat. Astronaut. Amsterdam, 1958, Bd. I, S. 343–358.
Molitz, H.: Einfluß des Luftwiderstandes auf die Bewegung von Satelliten. Wehrtech. Monatshefte 55, 593–607 (1958).
Nonweiler, T. R. P.: Perturbation of elliptic orbits by atmospheric contact. J. Brit. Interplanet. Soc. 16, 368–379 (1958).
Peterson, L. N.: Motion of a satellite with friction. ARS Journal 28, 750752 (1958).
Roberson, R. E.: Effect of air drag on elliptic satellite orbits. ARS Journal 28, 90–96 (1958).
Roberson, R. E.: Air drag effect on a satellite orbit described by difference equations in the revolution number. Quart. Appl. Math. 26, 131–136 (1958).
Williams, H. E.: The effect of drag on elliptic orbits. Adv. in Astronaut. Sci., Bd. 3, S. 35/1–10 (1958).
Baker, R. M. L. jr.: Application of astronomical perturbation techniques to the return of space vehicles. ARS Journal 29, 207–211 (1959).
Low, G. M.: Nearly circular transfer trajectories for descending satellites. NASA Tech. Rep. R-3 (1959).
Michielsen, H. F.: Orbit decay and prediction of the motion of artificial satellites. Adv. in Astronaut. Sci., Bd. 4, S. 255–310 (1959).
Rowell, L. N. und M. C. Smith: Secular variation in the inclination of the orbit of the earth satellite ( 1957 /3) and air drag. X. Kongr. Internat. Astronaut. London, 1959, Bd. I, S. 225–227.
Sterne, Th. E.: Effect of the rotation of a planetary atmosphere upon the orbit of a close satellite. ARS Journal 29, 777–782 (1959).
Gedeon, G. S.: Determination of the characteristics of rapidly decaying orbits. Adv. in Astronaut. Sci., Bd. 6, S. 458–472 (1960).
Batrakov, Yu. V. und V. P. Proskurin: Perturbations in the orbits of artificial satellites caused by air resistance. Artificial Earth Satellites 3, 56–66 (1961).
Braunbeck, W.: Das Satelliten-Paradoxon. Weltraumfahrt 12, 138–140 (1961).
El’yasberg, P. E.: Secular variations in orbit element as a function of air resistance. Artificial Earth Satellites 3, 76–84 (1961).
Kovalevsky, J.: Aspects analytiques du problème des perturbations d’un satellite artificiel. Astronaut. Acta 7, 376–389 (1961).
Vincent, Th. L.: Satellite life duration. ARS Journal 31, 1015–1018 (1961).
Billik, B.: Survey of current literature on satellite lifetimes. ARS Journal 32, 1641–1650 (1962).
Crisp, J. D. C.: The dynamics of supercircular multiple-pass atmospheric braking. Astronaut. Acta 8, 1–27 (1962).
Karrenberg, H. K. u. a.: Variation of satellite position with uncertainities in the mean atmospheric density. ARS Journal 32, 576–582 (1962).
Kork, J.: Satellite lifetimes in elliptic orbits. J. Aero. Sci. 29, 1273–1290, 1299 (1962).
Parsons, W. D.: Orbit decay characteristics due to drag. ARS Journal 32, 1876–1881 (1962).
Poor, J. G. and R. W. Dix: Vehicle dynamics considerations at parabolic velocities. ARS Journal 32, 1888–1891 (1962).
Brundin, C. L.: Effects of charged particles on the motion of an earth satellite. AIAA Journal 1, 2529–2538 (1963).
Citron, S. J.: Satellite lifetimes under the influence of continuous thrust, atmospheric drag and planet oblateness. AIAA Journal 1, 1355–1360 (1963).
Kalil, F.: Effect of an oblate rotating atmosphere on the eccentricity, semi-major axis, and period of a close earth satellite. AIAA Journal 1, 1872–1878 (1963).
Abdelkader, M. A.: Approximate orbits of resisted satellites. Astronaut. Acta 10, 328–338 (1964).
Denham, W. F. and A. F. Bryson jr.: Optimal programming problems with inequality constraints II: Solution by steepest-ascent. AIAA Journal 2, 25–34 (1964).
Lubowe, A. G.: Drag perturbations in low eccentricity orbits. Astronaut. Acta 11, 189–195 (1965).
Lawden, D. F.: Entry into circular orbits —1. J. Brit. Interplanet. Soc. 10, 5–17 (1951).
Lawden, D. F.: Inter-orbital transfer of a rocket. III. Kongr. Internat. Astronaut. Stuttgart, 1952, S. 146–161.
Lawden, D. F.: The calculation of orbits. J. Brit. Interplanet. Soc. 14, 204–214 (1955).
Ehricke, K. A.: The satelloid. Astronaut. Acta 2, 63–100 (1956).
Lawden, D. F.: Transfer between circular orbits. ARS Journal 26, 555–558 (1956).
Fried, B. D.: On the powered flight trajectory of an earth satellite. ARS Journal 27, 641–643 (1957).
Benney, D. J.: Escape from a circular orbit using tangential thrust. ARS Journal 28, 167–169 (1958).
Dobrowalski, A.: Micrithrust maneuver capabilities. Adv. in Astronaut. Sci., Bd. 3, S. 18/1–14 (1958).
Kelber, C. C.: Next: Maneuverable satellites. Adv. in Astronaut. Sci., Bd. 3, S. 17/1–18 (1958).
Lawden, D. F.: Optimal escape from a circular orbit. Astronaut. Acta 4, 218–233 (1958).
Vargo, L. G.: Optimal transfer between coplanar terminals in a gravitational field. Adv. in Astronaut. Sci., Bd. 3, S. 20/1–9 (1958).
Perkins, F. M.: Flight mechanics of low-thrust spacecraft. J. Aero. Sci. 26, 291–297 (1959).
Traenkle, C. A.: Optimal programming and control of satellite orbits. Z. Flugwiss. 7, 305–313 (1959).
Brunk, W. E.: Transfer between noncoplanar orbits without minimum bvelocity requirements. Adv. in Astronaut. Sci., Bd. 7, S. 111–124 (1960).
DeBra, D. B. and B. H. Gundel: Circularization of elliptic orbits. Adv. in Astronaut. Sci., Bd. 6, S. 536–555 (1960).
Godal, Th.: Conditions of compatibility of terminal positions and velocities. XI. Kongr. Internat. Astronaut. Stockholm, 1960, Bd. I, S. 40 11.
Lawden, D. F.: Optimal programme for correctional manoeuvres. Astronaut. Acta 6, 195–205 (1960).
Long, R. S.: Transfer between non-coplanar elliptical orbits. Astronaut. Acta 6, 167–178 (1960).
Munick, H. u. a.: Analytic solutions to several optimum orbit transfer problems. XI. Kongr. Internat. Astronaut. Stockholm, 1960, Bd. I, S. 423430.
Rider, L.: Ascent from inner circular to outer co-planar elliptic orbits. ARS Journal 30, 254–258 (1960).
Roberson, R. E.: Path control for satellite rendezvous. Adv. in Astronaut. Sci., Bd. 6, S. 192–228 (1960).
Soule, P. W.: Rendezvous with satellites in elliptical orbits with low eccentricity. Adv. in Astronaut. Sci., Bd. 7, S. 138–147 (1960).
Ting, Lu: Optimum orbital transfer by several impulses. Astronaut. Acta 6, 256–265 (1960).
Altman, S. P. and J. S. Pistiner: Hodograph analysis of the orbital transfer problem for coplanar nonaligned elliptical orbits. ARS Journal 31, 1217–1225 (1961).
Altman, S. P. and J. S. Pistiner: A new orbital rendezvous guidance concept and its mechanization. XII. Kongr. Internat. Astronaut. Washington, D. C., 1961, Bd. I, S. 254–272.
Breakwell, J. V. u. a.: Researches in interplanetary transfer. ARS Journal 31, 201–208 (1961).
Bruce, R. W.: Satellite orbit sustaining techniques. ARS Journal 31, 1237–1241 (1961).
Carstens, J. P. and T. N. Edelbaum: Optimum maneuvers for launching satellites into circular orbits of arbitrary radius and inclination. ARS Journal 31, 943–949 (1961).
Faulders, C. R.: Minimum time steering programs for orbital transfer with low-thrust rockets. Astronaut. Acta 7, 35–49 (1961).
Haynes, G. W.: The calculus of variations approach to the general optimum impulsive transfer problem. XII. Kongr. Internat. Astronaut. Washington, D. C., 1961, Bd. I, S. 299–316.
Houbolt, J. C.: Problems and potentialities of space rendezvous. Astronaut. Acta 7, 406–429 (1961).
Lass, H. and J. Lorell: Low acceleration takeoff from a satellite orbit. ARS Journal 31, 24–28 (1961).
Nason, M. L.: A terminal guidance law wich achieves collision based on Coriolis-balance techniques. Adv. in Astronaut. Sci., Bd. 8, S. 439–461 (1961).
Smith, F. T.: Optimization of multistage orbit transfer processes by dynamic programming. ARS Journal 31, 1553–1559 (1961).
Traenkle, C. A.: Layout of satellite ferry operation. Z. Flugwiss. 9, 334–341 (1961).
Traenkle, C. A.: Ferry operation with elliptic satellite orbits. Z. Flugwiss. 9, 407–417 (1961).
Young, J. W. u. a.: Guidance of a space vehicle to a desired point on the earth’s surface. Adv. in Astronaut. Sci., Bd. 8, 5. 46–474 (1961).
Dierstein, R.: Aufstiegs- and Übergangsbahnen. WGL-Lehrgang fur Raumfahrttechnik (München 1962) Bd. II, 16–1/22.
Eckel, K.: Optimum transfer between non-coplanar elliptical orbits. Astronaut. Acta 8, 177–192 (1962).
Fosdick, G. E. and M. L. Anthony: Three-dimensional pulse optimization for vehicles desorbiting from circular orbits. Astronaut. Acta 8, 343–375 (1962).
Gobetz, F. W.: Optimal variable-thrust transfer of a power-limited rocket between neighboring circular orbits. ARS Journal 32, 339–343 (1962).
Horner, J. M.: Optimum two-impulse transfer between arbitrary coplanar terminals. ARS Journal 32, 95–96 (1962).
Jantscher, H. N. u. a.: Minimum energy analysis for the general problem of rendezvous in earth orbital space. ARS Journal 32, 292–294 (1962).
Jurovics, S. A. and J. E. McIntyre: The adjoint method and its application to trajectory optimization. ARS Journal 32, 1354–1358 (1962).
Lass, H. and C. B. Solloway: Motion of a satellite under the influence of a constant normal thrust. ARS Journal 32, 97–100 (1962).
Lawden, D. F.: Optimal intermediate-thrust arcs in a gravitational field. Astronaut. Acta 8, 106–123 (1962).
Lieberman, S. I.: Rendezvous acceptability regions based on energy considerations. ARS Journal 32, 287–290 (1962).
London, H. S.: Change of satellite orbit plane by aerodynamic maneuvering. J. Aero. Sci. 29, 323–332 (1962).
Melbourne, W. G. and C. G. Sauer jr.: Optimum thrust programs for power-limited propulsion systems. Astronaut. Acta 8, 205–227 (1962).
Munick, H.: Optimum orbital transfer using N-impulses. ARS Journal 32, 1347–1350 (1962).
Regan, F. J.: Comment on an orbital hodograph analysis by Altman and Pistiner. ARS Journal 32, 113–114 (1962).
Roberson, R. E.: An intermittent orbit sustaining technique. Astronaut. Acta 8, 42–48 (1962).
Weiss, D. C.: Maneuvring technique for changing the plane of circular orbits with minimum fuel expenditure. J. Aero. Sci. 29, 368–369 (1962).
Anthony, M. L. and G. E. Fosdick: Three-dimensional pulse optimization for vehicles disorbiting from elliptical orbits. Astronaut. Acta 9, 81–106 (1963).
Barrar, R. B.: An analytic proof that the Hohmann-type transfer is the true minimum two-impulse transfer. Astronaut. Acta 9, 1–11 (1963).
Barrar, R. B.: Two-impulse transfer vs. one-impulse transfer: analytic theory. AIAA Journal 1, 65–68 (1963).
Billik, B. H. and C. M. Price: Preferred schemes for multiple orbit transfer. AIAA Journal 1, 1858–1861 (1963).
Bryson, A. E. jr. u. a.: Optimal programming problems with inequality constraints. I: Necessary conditions for extremal solutions. AIAA Journal 1, 2544–2550 (1963).
Eckel, K.: Optimum transfer in a central force field with n impulses. Astronaut. Acta 9, 302–324 (1963).
Eckel, K.: Numerical solutions of non-coaxial optimum transfer problems. J. Astronaut. Sci. 10, 82–92 (1963).
Fimple, W. R.: An improved theory of the use of high- and low-thrust propulsion in combination. J. Astronaut. Sci. 10, 107–113 (1963).
Gobetz, F. W.: Optimum transfers between hyperbolic asymptotes. AIAA Journal 1, 2034–2041 (1963).
Hanson, J. N.: A simple method for approximating the optimal trajectory. AIAA Journal 1, 1936–1938 (1963).
Hinz, H. K.: Optimal low-thrust near-circular orbital transfer. AIAA Journal 1, 1367–1371 (1963).
Kelley, H. J.: Singular extremals in Lawden’s problem of optimal rocket flight. AIAA Journal 1, 1578–1580 (1963).
Kooy, J. M. J.: On ascent guidance for rendezvous. Astronaut. Acta 9, 140–166 (1963).
McCue, G. A.: Optimum two-impulse orbital transfer and rendezvous between inclined elliptical orbits. AIAA Journal 1, 1865–1872 (1963).
Moskowitz, S. E.: On the accuracy of approximate thrust steering schedules in optimal correctional maneuvers. Astronaut. Acta 9, 20–30 (1963).
Sconzo, P.: An astronomical approach to the problem of satellite rendezvous. Astronaut. Acta 9, 367–370 (1963).
Ting, Lu and M. Pierucci: Optimum launching of a satellite by two impulses of unequal specific impulse. Astronaut. Acta 9, 174–183 (1963).
Wang, K.: Minimum time transfer between coplanar, circular orbits by two impulses and the propulsion requirements. Astronaut. Acta 9, 12–19 (1963).
Zee, C.H.: Low-thrust oscillatory spiral trajectory. Astronaut. Acta 9, 201–207 (1963).
Zee, C.-H.: Low constant tangential thrust spiral trajectories. AIAA Journal 1, 1581–1583 (1963).
Zee, C.-H.: Effect of finite thrusting time in orbital maneuvers. AIAA Journal 1, 60–64 (1963).
Auelmann, R. R.: Trajectories with constant normal force starting from a circular orbit. AIAA Journal 2, 561–563 (1964).
Billik, B. H.: Some optimal low-acceleration rendezvous maneuvers. AIAA Journal 2, 510–516 (1964).
Edelbaum, Th. N.: Optimum low-thrust rendezvous and station keeping. AIAA Journal 2, 1196–1201 (1964).
Grabin, C.: Docking dynamics for rigid-body spacecraft. AIAA Journal 2, 5–12 (1964).
Hempel, P. und J. Tschauner: Über Beschleunigungsprogramme minimaler Übergangsenergie für das Rendezvous-Manöver. Astronaut. Acta 10, 221–237 (1964).
Lee, G.: An analysis of two-impulse orbital transfer. AIAA Journal 2, 1767–1773 (1964).
McGill, R. und P. Kenneth: Solution of variational problems by means of a generalized Newton-Raphson operator. AIAA Journal 2, 1761–1766 (1964).
Metzger, R.: Anwendung des Pontrjaginschen Maximumprinzips auf Rendezvousprobleme in der Raumfahrt. Jahrbuch 1964 der WGLR, S. 233–237.
Peterson, E. L.: Methods and application of optimization techniques. AGARDograph 92 (Okt. 1964 ), S. 109–162.
Smith, F. T.: The application of dynamic programming to orbit transfer processes. AGARDograph 92 (Okt. 1964 ), S. 22–78.
Tschauner, J. und P. Hempel: Optimale Beschleunigungsprogramme für das Rendezvous-Manöver. Astronaut. Acta 10, 296–307 (1964).
Vinh, N. X.: A property of cotangential elliptical transfer orbits. AIAA Journal 2, 1841–1844 (1964).
Anthony, M. L. und F. T. Sasaki: Rendezvous problem for nearly circular orbits. AIAA Journal 3, 1666–1673 (1965).
Bruce, R. W.: Combined aerodynamic-propulsive orbital plane change maneuver. AIAA Journal 3, 1286–1289 (1965).
Busemann, A.: Minimalprobleme der Luft- und Raumfahrt. Z. Flugwiss. 13, 401–411 (1965).
Conrad, D. A.: Minimum fuel closed loop translation. AIAA Journal 3, 952–954 (1965).
Edelbaum, Th. N.: Optimum power-limited orbit transfer in strong gravity fields. AIAA Journal 3, 921–925 (1965).
Johnson, D. P.: Perturbation solutions for low-thrust rocket trajectories. AIAA Journal 3, 1934–1936 (1965).
Marchai, C.: Transferts optimaux entre orbits elliptiques coplanaires (durée indifférente). Astronaut. Acta 11, 432–445 (1965).
Marec, J.-P.: Transferts orbitaux économiques. Recherche Aérospatiale Nr. 105, 11–21 (1965).
McCue, G. A. und D. F. Bender: Numerical investigation of minimum impulse orbital transfer. AIAA Journal 3, 2328–2334 (1965).
Moyer, H. G.: Minimum impulse coplanar circle-ellipse transfer. AIAA Journal 3, 723–726 (1965).
Pfeiffer, C. G.: A dynamic programming analysis of multiple guidance corrections of a trajectory. AIAA Journal 3, 1674–1681 (1965).
Pierucci, M.: Optimum orbital transfer by two impulses of unequal specific impulse. Astronaut. Acta 11, 268–270 (1965).
Robbins, H. M.: Optimality of intermediate-thrust arcs of rocket trajectories. AIAA Journal 3, 1094–1098 (1965).
Tschauner, J. und P. Hempel: Rendezvous zu einem in elliptischer Bahn umlaufenden Ziel. Astronaut. Acta 11, 104–109 (1965).
Tschauner, J.: Neue Darstellung des Rendezvous bei elliptischer Zielbahn. Astronaut. Acta 11, 312–321 (1965).
Vaccaro, R. J. und M. J. Kirby: Rendezvous guidance of lifting aerospace vehicles. J. Spacecraft 2, 705–711 (1965).
de Veubeke, B. Fraeijs: Canonical transformations and the thrust — coast — thrust optimal transfer problem. Astronaut. Acta 11, 271–282 (1965).
Zehle, H.: Zur Berechnung von Abflugspiralen kleiner Schubbeschleunigung. Z. Flugwiss. 13, 385–387 (1965).
Author information
Authors and Affiliations
Rights and permissions
Copyright information
© 1969 Friedr. Vieweg & Sohn GmbH, Braunschweig
About this chapter
Cite this chapter
Stümke, H. (1969). Flugleistungen der drehsymmetrischen Flugkörper. In: Grundzüge der Flugmechanik und Ballistik. Vieweg+Teubner Verlag, Wiesbaden. https://doi.org/10.1007/978-3-663-07250-8_5
Download citation
DOI: https://doi.org/10.1007/978-3-663-07250-8_5
Publisher Name: Vieweg+Teubner Verlag, Wiesbaden
Print ISBN: 978-3-663-06337-7
Online ISBN: 978-3-663-07250-8
eBook Packages: Springer Book Archive