Abstract
In this chapter a catalogue of time-optimal low-thrust transfers from arbitrary departure orbits to the geostationary orbit is constructed. This catalogue is obtained by solving a multitude of optimal control problems with a combination of simple and multiple shooting techniques, augmented by a multi-dimensional homotopy. Modified equinoctial elements are used to describe the satellite dynamics, and state-of-the-art values for thrust and specific impulse are considered. The ultimate outcome consists of a synthetic law for transfer time, and thus cost, as function of the orbit injection parameters and engine figures. This law can be consulted in the early stages of mission design.
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Arianespace: Ariane 5 User’s Manual (Issue 3 - Revision 0) (2000)
Arianespace: Ariane 6 User’s Manual (Issue 0 - Revision 0) (2016)
Bryson, A., Ho, Y.: Applied Optimal Control. Wiley, New York (1975)
Caillau, J.B.: Contribution à l’étude du contrôle en temps minimal des transferts orbitaux. Ph.D. dissertation, Institut National Polytechnique de Toulouse (2000)
Caillau, J.B., Daoud, B.: Minimum time control of the restricted three-body problem. SIAM J. Control Optim. 50, 3178–3202 (2012)
Caillau, J.B., Noailles, J.: Coplanar control of a satellite around the Earth. ESAIM Control Optim. Calc. Var. 6, 239–258 (2001)
Casalino, L., Colasurdo, G.: Improved Edelbaum’s approach to optimize low earth/geostationary orbits low-thrust transfers. J. Guid. Control Dyn. 30, 1504–1511 (2007)
Ceccherini, S., Topputo, F.: System-trajectory optimization of hybrid transfers to the geostationary orbit. In: Proceedings of 2018 Space Flight Mechanics Meeting, AIAA SciTech Forum, Kissimmee, FL, 8–12 January 2018
Ceccherini, S., Ferella, L., Topputo, F.: Assessment of hybrid propulsion for geostationary transfer orbit: a mission design approach. In: Proceedings of the 67th International Astronautical Congress (IAC 2015), Guadalajara, 26–30 September 2016
Cefola, P.J.: Equinoctial orbit elements–application to artificial satellite orbits. In: Proceedings of AIAA/AAS Astrodynamics Conference, AIAA 72-937, Palo Alto, CA, 11–12 September 1972
Edelbaum, T.N.: Propulsion requirements for controllable satellites. ARS J. 31, 1079–1089 (1961)
Edelbaum, T., Sackett, L., Malchow, H.: Optimal low thrust geocentric transfer. In: Proceedings of AIAA 10th Electric Propulsion Conference, AIAA 73-1074, Lake Tahoe, NV, October 31–November 2 1973
Goebel, D.M., Katz, I.: Fundamentals of Electric Propulsion: Ion and Hall thrusters. Wiley, New York (2008)
Gonzalo, J.L., Topputo, F., Armellin, R.: Indirect optimization of end-of-life disposal for Galileo constellation using low thrust propulsion. In: Proceedings of the 26th International Symposium on Space Flight Dynamics, Matsuyama, 3–9 June 2017
Graham, K.F., Rao, A.V.: Minimum-time trajectory optimization of multiple revolution low-thrust Earth-orbit transfers. J. Spacecr. Rockets 52, 711–727 (2015)
Haberkorn, T., Martinon, P., Gergaud, J.: Low thrust minimum-fuel orbital transfer: a homotopic approach. J. Guid. Control Dyn. 27, 1046–1060 (2004)
Kechichian, J.A.: Optimal low-earth-orbit-geostationary-earth-orbit intermediate acceleration orbit transfer. J. Guid. Control Dyn. 20, 803–811 (1997)
Kechichian, J.A.: Reformulation of Edelbaum’s low-thrust transfer problem using optimal control theory. J. Guid. Control. Dyn. 20, 988–994 (1997)
Kluever, C.A.: Using Edelbaum’s method to compute low-thrust transfers with earth-shadow eclipses. J. Guid. Control Dyn. 34, 300–303 (2001)
Kluever, C.A.: Designing transfers to geostationary orbit using combined chemical-electric propulsion. J. Spacecr. Rockets 52, 1144–1151 (2015)
Kluever, C.A., Oleson, S.R.: Direct approach for computing near-optimal low-thrust Earth-orbit transfers. J. Spacecr. Rockets 35, 509–515 (1998)
Martinon, P., Gergaud, J.: SHOOT2.0: an indirect grid shooting package for optimal control problems, with switching handling and embedded continuation. Research Report 7380, INRIA (2010)
Pan, B., Lu, P., Pan, X., Ma, Y.: Double-homotopy method for solving optimal control problems. J. Guid. Control Dyn. 39, 1706–1720 (2016)
Pontryagin, L.: Mathematical Theory of Optimal Processes, pp. 1–114. Interscience, New York (1962)
Zhang, C., Topputo, F., Bernelli-Zazzera, F., Zhao, Y.S.: Low-thrust minimum-fuel optimization in the circular restricted three-body problem. J. Guid. Control Dyn. 38, 1501–1510 (2015)
Acknowledgements
The authors would like to acknowledge Natividad Ramos Morón whose MSc Thesis inspired the work described in this chapter and Juan Luis Gonzalo for reviewing LT2O and making it more efficient.
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Topputo, F., Ceccherini, S. (2019). A Catalogue of Parametric Time-Optimal Transfers for All-Electric GEO Satellites. In: Fasano, G., Pintér, J. (eds) Modeling and Optimization in Space Engineering . Springer Optimization and Its Applications, vol 144. Springer, Cham. https://doi.org/10.1007/978-3-030-10501-3_17
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