A Minimum-Fuel Fixed-Time Low-Thrust Rendezvous Solved with the Switching Systems Theory
Author:
Affiliation:
1. LAAS-CNRS, Université de Toulouse, CNRS
2. CNES, Centre Spatial de Toulouse
3. Thales Alenia Space
Publisher
Japan Society for Aeronautical and Space Sciences
Link
https://www.jstage.jst.go.jp/article/tastj/16/7/16_628/_pdf
Reference15 articles.
1. 1) Euler, E. A.: Optimal Low-Thrust Rendezvous Control, AIAA Journal, 7 (1969), pp. 1140–1144.
2. 2) Lawden, D. F.: Optimal Trajectories for Space Navigation, Butterwort edition, London, 1963.
3. 3) Dankanich, J. W.: Low-Thrust Mission Design and Application,AIAA Paper 2010-6857, 2010.
4. 4) Feng, W., Wang, B., Yang, K., and Zhao, D.: Cooperative Rendezvous between two Spacecraft under Finite Thrust, CEAS Space J., 9 (2017), pp.227–241.
5. 5) Serra, R., Arzelier, D., Rondepierre, A., and Calvet, J.-L.: Analytical Optimal Solutions of Impulsive Out-of-plane Rendezvous around Elliptic Orbits, IFAC-PapersOnLine, 19 (2014), pp. 2231–2236.
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