Zusammenfassung
Verschiedene technische Forderungen und Beschränkungen machen es erforderlich, den Flugablauf von Raumfahrzeugen bei der Erfüllung einer Mission auf lange Sicht zu planen und ein Flugprogramm für das Lenksystem herzustellen. Diesen Vorgang nennt man Navigation.
This is a preview of subscription content, log in via an institution.
Buying options
Tax calculation will be finalised at checkout
Purchases are for personal use only
Learn about institutional subscriptionsPreview
Unable to display preview. Download preview PDF.
Literatur
Albright, N. W., The Transformation of Earth — Referenced Data to Inertial Coordinate Systems, Jet Propulsion Lab., Pasadena, Cal., Progress-Report No. 30–5, 1959.
Altmann, S. P., und J. S. Pistinger, Hodograph Analysis of the Orbital Transfer Problem for Coplanar Nonaligned Elliptical Orbits, J. ARS, 31 (9), 1961.
Arthur, P. D., und H. K. Karrenberg, Simple Method for Approximation of the Characteristics of Low Thrust Trajectories, J. ARS, 30 (7), 1960.
Au, G., Interplanetare Bahnen mit kleiner Schubbeschleunigung, Raketentechnik und Raumfahrtforschung, 5 (2), 1961.
Baker, R. M. L., Application of Astronomical Perturbation Techniques to the Return of Space Vehicles, Jet Propulsion, 29 (3), 1959.
Baker, R. M. L., Accuracy Required for a Return from Interplanetary Voyages, J. BIS, 17 (3/4), 1959/60.
Baker, R. M. L., G. B. Westrom, C. B. Hilton, R. H. Gersten, J. L. Arsenault, und E. J. Browne, Efficient Precision Orbit Computation Techniques, J. ARS, 30 (8), 1960.
Battin, R. H., A Comparison of Fixed and Variable Time of Arrival Navigation for Interplanetary Flight, Massachusetts Institute of Techniques, Mai 1960, A STIA AD — 242 862.
Battik, R. H., und J. H. Lanning, A Navigation Theory for Round Trip Recounaissance Missions for Venus and Mars, 4 Sympos. on Ball. Missiles and Space Technology, 24.-27. Aug. 1957, UCLA, Los Angeles.
Bennet, D. J., Escape from a circular Orbit Using Tangentical Thrust, Jet Propulsion, 28 (3), 1958.
Boyd, B., Motion Units for Simplify Space Travel Computations, J. ARS, 29 (3), 1959.
Breakwell, J. V., Approximations in Flight Optimization Problems, Aerospace Eng., 20 (9), I, 1961.
Breakwell, J. V., Gillespie und Ross, Researches in Interplanetary Transfer, J. ARS, 31 (2), 1961.
Brown, H., und J. R. Nelson, Thrust Orientation Patterns for Orbit Adjustment of Low Thrust Vehicles, J. ARS, 30 (7), 1960.
Cap, F., Die Anwendung der Gröbnerschen Methode zur Lösung von Differentialgleichungen des astronautischen n-Körper-Problems, Proc. IX. Internat. Astronaut. Congress, Wien 1959, Springer.
Clarke, V. C. jr., Design of Lunar and Interplanetary Ascent Trajectories, Jet Propulsion Lab., 26. 7. 1960, ASTIA AD — 246 430.
Cole, D. M., Times Required for Continous Thrust Earth Moon Trips, J. ARS, 27 (4), 1957.
Copland, H., Interplanetary Trajectory under Low Thrust Radial Acceleration, J. ARS, 29 (4), 1959.
Cornog, R., Selected Problems in Interstellar Navigation. Institute of Navigation, 7 (2 + 3), 1960.
Crocco, G. A., One Year Exploration Trip Earth—Mars—Venus—Earth, Prod. 7. Intern. Astronaut. Congr., Wien 1957, Springer.
Don Gray, J., Drag and Stability Derivatives of Missile Components According to the Modified Newtonian Theory, ASTIA AD — 246 085, 1960.
Dobranravov, V., Kosmische Navigation, Naukai Zhizu, 23 (10) 1956, (russisch).
Dugan, J. F. jr., Analysis of Trajectory Parameters for Probe and Round-TripMissions to Mars, NASA TN D — 281, 1960.
Eggleston, J. M., Optimum Time to Rendezvous, J. ARS, 30 (11), 1960.
Ehricke, K. A., Space Flight, Princetown, N. J., 1960, Van Norstrand Comp., Inc.
Ehricke, K. A., Take-off from Satellite Orbits, J. ARS, 23 (6), 1953.
Ehricke, K. A., Zur Auswahl von Flugbahnen für bemannte Raumfahrzeuge zu den Planeten Mars und Venus, Raketentechnik und Raumfahrtforschung, 4 (1), 1960.
Ehricke, K. A., Interplanetary Probes, Astronautics, Jan. 1959.
Ehricke, K. A., Error Analysis at Keplerian Flights Involving Single Central Force Field between two Central Force Fields, Navigation, 6 (1), 1956.
Forbes, G. F., The Trajectory of a Powered Rocket in Space, J. BIS, 9 (2), 1950.
Fox, R. H., Powered Trajectory Studies for Low Thrust Space Vehicles, ARS Paper, 879–59, New York 1959.
Fried, B. D., Trajectory Optimization Problems, in: Seifert, Space Technology, New York 1959, John Wiley and Sons, Inc.
Fried, B. D., On the Powered Flight Trajectory of an Earth Satellite, J. ARS, 27 (6), 1957.
Gravalos, P. G., A Method of Integrating the Equations of Motion of a Body Entering an Arbitrary Atmosphere with an Automatic Error Analysis, Proc. VIII. Internat. Astr. Congr., Wien 1957, Springer.
Greenwood, S. W., Solar Sailing — Practical Problems, Jet Propulsion, 28 (11), 1958.
Greenwood, S. W., Minimum Energy Entry into Orbits Around Mercury, J. BIS, 18 (4), 1961.
Gröbner, W., und F. Cap, The Three-Body Problem Earth — Moon — Spaceship, Astronautica Acta, Vol. V, Fasc. 5, 1959.
Harcrow, H. W., Optimum Trajectory of n-Stage-Missiles, J. BIS, 18 (2) 1961.
Harry, D. P., und A. L. Friedlander, An Analysis of Errors and Requierements for Optical Guidance Technique for Approaches to Atmosphere Entry with Interplanetary Vehicles, NASA TR — 102, 1961.
Herricx, S., R. M. L. Baker und C. G. Hilton, Gravitational and Related Constants for Accurate Space Navigation, Proc. VIII. Int. Astronaut. Congr., Wien 1957, Springer.
Himmel, S. C., J. F. Dugan, R. W. Luidens und R. F. Weber, A Study of Manned Nuclear — Rocket Missions to Mars, Aerospace Eng., 20 (7), 1961.
Hirrel, P. J., Control and Guidance of Electrically Propelled Spacecraft, Calif. Inst. Tech., JPL TR — 32–166, Sept. 1961.
Hohmann, W., The Attainability of Heavenly Bodies, NASA Technical Trans. No. F — 44, 1960. — ASTIA AD — 246 795 (Nachdruck von »Die Erreichbarkeit der Himmelskörper«, 1925 ).
Huang, Su-Situ, Very Restricted Four-Body Problem, NASA TND — 501, September 1960.
Hunter, M. W., W. B. Klempererund R. J. Gunkel, Impulsive Midcourse Correction of a Lunar Shot, Proc. IX. Int. Astronaut. Congr., Wien 1959, Springer.
Irving, J. H., und E. K. Blum, Comparative Performance of Ballistie and Low Thrust Vehicles for Flight to Mars, 2. Annual AFOSR Symposium, Denver 1958; Vistas in Astronautics, Vol. II, Pergamon Press, 1959.
Koelle, H. H. (ed.), Handbook of Astronautical Engineering, New York 1961, McGraw-Hill Book Comp., Inc.
Knothe, H., und R. H. Anderson, On Satellite Orbits, AFMDC — TR — 59–11, April 1959. — A STIA AD — 211 523.
Koor, J. M. J., On the Calculation of the Powered Flight of a long Range Rocket Superviset by an Automatic Pilot, Astronautica Acta, 1 (4), 1955.
Kosmodem’yanskill, A. A., General Theorems of the Mechanics of a Body of Variable Mass, Jzd. VVIV, 1946 (russisch).
Kosmodem’yanskii, A. A., Mechanics of Bodies of Variable Mass; Theory of Jet Propulsion, Jzd. VVIA, 1957 (russisch).
Krause, H. G. L., zum Problem: Die Bahnbestimmung aus dem Vektor der Bahngeschwindigkeit und der Einfluß einer Änderung derselben auf die Bahnelemente, Weltraumfahrt, Heft 2, 1954.
Landolt-Börnstein, Zahlenwerte und Funktionen aus Astronomie und Geophysik, Heidelberg 1952, Springer.
Lass und Solloway, Method of a Satellite of the Moon, J. ARS, 31 (2), 1961.
Lawden, D. F., Optimal Intermediate-Thrust Areas in a Gravitational Field, Astronautica Acta, V III, 1962.
Lawden, D. F., Optimal Programming of Rocket Thrust Directions, Astronautica Acta, I, 1955.
Lawden, D. F., The Calculation of Orbits, J. BIS, 14 (4), 1955.
Lawden, D. F., Optimal Rocket Trajectories, J. ARS, 27 (12), 1957.
Lawden, D. F., Lagrange’s Equations for a System of Variable Mass, J. BIS, 6 (6), 1947.
Lawden, D. F., und R. S. Long, The Theory of Correctional Maneuvers in Interplanetary Space, Radiation Inc., Aug. 1960, ASTIA AD — 242 394.
Leger, R. M., Effects of Launching Time on Space Navigation, 7 (4), 1960.
Melbourne, W. G., Three-Dimensional Optimum Thrust Trajekties for Power Limited Propulsion Systems, J. Ars, 31, 1961.
Michielsen, H. F., The Case for the Low Acceleration Spaceship, Astronautica Acta, 3 (2), 1957.
Michielsen, H. F., Die Bahnbestimmung einer schwach beschleunigten Rakete in einem zentralen Schwerefeld, in: H. H. Koelle (ed.), Probleme der astronaut. Grundlagenforschung, 1952.
Michielsen, H. F., Fifth Harmonic of Earth’s Gravitational Field, J. ARS, 30 (10), 1960.
Micxelwarr, A. B., Lunar Trajectories, J. ARS, 29 (12) 1959.
Mickelwait, A. B., E. H. Timpeins und R. A. Park, Three Dimensional Interplanetary Trajectories, IRE Trans. MIL — 3, No. 4, 1959.
Miele, A., General Variational Theory of the Flight Paths of Rocket Powered Aircraft, Missiles and Satellite-Carriers, Proc. 9. Int. Astronaut. Congr., Vol. II, Wien 1959, Springer.
Miele, A., Optimum Burning Program as Related to Aerodynamic Heating for a Missile Traversing the Earth’s Atmosphere, J. ARS, 27 (10), 1957.
Miele, A., Interrelationship of Calculus of Variations and Ordinary Theory of Maxima and Minima for Flight Mechanies Application, J. Ars, 29 (1), 1959.
Miele, A., Generalized Variotional Approach to the Optimum Thrust Programming for the Vertical Flight of a Rocket, Z. Flugwissenschaft, März 1958.
Miele, A., Theorem of Image Trajectories in the Earth-Moon-Space, A STIA AD — 245 790, 1960.
Moeckel, W. E., Fast Interplanetary Missions with Law — Thrust Propulsion Systems, NASA TR R — 79, 1960.
Moeckel, W. E., Trajectories with Constant Tangential Thrust in Central Gravitational Field, NASA TRR — 53, 1959.
Moeckel, W. E., Interplanetary Trajectories for Elektrically Propelled Space Vehicles, Astronautica Acta, 7, 1961.
Ocnocimskij, D. E., und T. M. Eneev, Einige Variationsaufgaben zum Start eines künstlichen Erdsatelliten, USP. fiz. Nauk (Moskau), 63, 1957.
Paiewonsky, B., The Motion of an Orbiting Vehicle Subjected to Continuous Radial Thrust, Including a Study of Planetary Encaunters, Proc. X. Int. Astronaut. Congr., Vol. I, Wien 1960, Springer.
Pauson, W. M., Time Relationships for Interplanetary Trajectories, J. ARS, 31 (9), Sep. 1961.
Perkins, F. M., Flight Mechanics of Low — Thrust Spacecraft, in: Vistas in Astronautics, Vol. II, London 1959, Pergamon Press.
Petty, C. M., Interplanetary Maneuvers Using Radial Thrust, J. ARS, 31, 1961.
Rauschenbach, B. V., Some Guidance Problems in Interplanetary Space, J. ARS, 31, 1961.
Ridell, W. C., Launch Parameters for Interplanetary Flights, J. ARS, 30 (12), 1960.
Ridell, W. C., Initial Azimuths and Times for Ballistie Lunar Impact Trajectories, J. ARS, 30 (5), 1960.
Roberson, R. E., Impact Points of Ballistie Rockets, J. ARS, 27 (12), 1957.
Roberson, R. E., und D. Tatisrcheff, The Potential Energy of a Small Rigid Body in the Gravitational Field of an Oblate Spheroid, J. Franklin Inst., 262, 1956.
Rodrignez, E., A Method of Determining Steering Programs for Low Thrust Planetary Vehicles, ARS Paper 645–58, 1958.
Rodrignez, E., Method for Determing Steeringining Programs for Low Thrust Interplanetary Vehicles, J. ARS, 29 (10), 1959.
Roth, H. L., Transfer from an Arbitrary Initial Flight Condition to a Point Target, J. Aerospace Sci., 28 (9), 1961.
Ruppe, H. O., Einige Betrachtungen zur Theorie der Raumfahrzeugantriebe, Proc. VII Int. Astronaut. Congr., Wien 1957, Springer.
Ruppe, H. O., Satellite Technology and Space Navigation, ABMA Report No. DSP-TN-9–58, Sep. 1958.
Saltzer, C., und C. W. Fetheroff, A Direct Variotional Method for the Calenlation of Optimum Thrust Programs for Power — Limited Interplanetary Flight, Astronautica Acta, 7 (1), 1961.
Sänger, E., Bewegungsgesetze der Raumfahrt, Interavia, 4, 1949.
Sänger, E., Atlas konkreter Bahnen von Raketenflugzeugen bis zur Außenstation, Bericht No.3 derNordwestdeutschenGesellschaft fürWeltraumforschung e. V.,1951.
Schaub, W., Ein streng lösbarer Fall des Drei-Körper-Problems, Weltraumfahrt, Heft 3, 1957.
Schütte, K., Die Bahnbestimmung aus dem Vektor der Bahngeschwindigkeit und der Einfluß einer Änderung derselben auf die Bahnelemente, Weltraumfahrt, Heft 4, 1953, und Heft 1, 1954.
Sinra, J., Interplanetary Navigation, Proc. X. Int. Astronaut. Congr., Vol. II, Wien 1960, Springer.
Stark, H. M., Optimal Trajectories Between Two Terminals in Space, J. ARS, 31 (2), 1961.
Stuhlinger, E., The Flight Path of an Electrically Propelled Space Ship, J. ARS, 27 (4), 1957.
Thirring, H., Der Einfluß der Eigenrotation der Planeten auf die Bewegung ihrer Trabanten, Physikal. Blätter, 5, 1958.
Traenkle, C. A., Design Parameters and Optimization of Missile Trajectories, Wadc Report 58–580, Astia AD — 204 805, 1958.
Tsien, H. S., Take-Off from Satellite Orbit, J. ARS, 23 (4), 1953.
Tsu, T. C., Interplanetary Travel by Solar Sail, J. ARS, 29 (6), 1959.
Unger, H. W., On the Mid-Course Navigation for Manned Interplanetary Space Flight, ABMA-Report, 28. 8. 1958, DSP — TR — 2–58.
Vertregt, M., Die Bahnbestimmung aus dem Vektor der Bahngeschwindigkeit, Astronautica Acta, 4 (1), 1958.
Vinti, J. P., Mean Motion in Conditionally Periodic Separable Systems, ASTIA AD — 246 592, Nov. 1960.
Weiss, D. C., Maneuvering Technique for Changing the Plane of Circular Orbits With Minimum Full Expenditure, J. Aerospace Sci., 29 (3), 1962.
Wen, Li Shu, A Unified Treatment of »Variation of Parameters« and »Differential Expressions«, Method in Trajectory Prediction and Error Analysis, J. Aerospace Sci., 29 (1), 1962.
Wu, Ching-Sheng, Effect of Earth’s Oblateness on the Calenlation of the Impact Point of Ballistie Missiles J. ARS, 30 (12), 1960.
Author information
Authors and Affiliations
Rights and permissions
Copyright information
© 1963 Springer Fachmedien Wiesbaden
About this chapter
Cite this chapter
Rößger, E., Zehle, H. (1963). Navigation. In: Grundlagen der Raumfahrzeugführung. Forschungsberichte des Landes Nordrhein-Westfalen, vol 1258. VS Verlag für Sozialwissenschaften, Wiesbaden. https://doi.org/10.1007/978-3-663-02530-6_2
Download citation
DOI: https://doi.org/10.1007/978-3-663-02530-6_2
Publisher Name: VS Verlag für Sozialwissenschaften, Wiesbaden
Print ISBN: 978-3-663-00617-6
Online ISBN: 978-3-663-02530-6
eBook Packages: Springer Book Archive