Spacecraft Rendezvous Using Constant-Magnitude Low Thrust

[1] Alfriend K., 2009, SPACECRAFT FORMATION, P185, DOI [10.1016/C2009-0-17485-8, DOI 10.1016/C2009-0-17485-8]

[2] Optimal servicing of geosynchronous satellites [J]. JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2006, 29 (01) : 203 - 206

[3] TIME-, FUEL-, AND ENERGY-OPTIMAL CONTROL OF NONLINEAR NORM-INVARIANT SYSTEMS [J]. IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 1963, : 196 - &

[4] Optimal power-limited rendezvous with upper and lower bounds on thrust [J]. JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1996, 19 (05) : 1124 - 1133

[5] TERMINAL GUIDANCE SYSTEM FOR SATELLITE RENDEZVOUS [J]. JOURNAL OF THE AEROSPACE SCIENCES, 1960, 27 (09): : 653 - &

[6] Fehse W., 2003, Automated Rendezvous and Docking of Spacecraft, P8, DOI [10.1017/CBO9780511543388, DOI 10.1017/CBO9780511543388]

[7] Minimum-Time Trajectory Optimization of Low-Thrust Earth-Orbit Transfers with Eclipsing [J]. JOURNAL OF SPACECRAFT AND ROCKETS, 2016, 53 (02) : 289 - 303

[8] CONTROLLABILITY MINIMUM PRINCIPLE [J]. JOURNAL OF OPTIMIZATION THEORY AND APPLICATIONS, 1975, 17 (1-2) : 93 - 114

[9] Gurfil P, 2016, ASTROPHYS SPACE SC L, V436, P1, DOI 10.1007/978-3-662-50370-6

[10] Nonlinear feedback control of low-thrust orbital transfer in a central gravitational field [J]. ACTA ASTRONAUTICA, 2007, 60 (8-9) : 631 - 648

[1] Alfriend K., 2009, SPACECRAFT FORMATION, P185, DOI [10.1016/C2009-0-17485-8, DOI 10.1016/C2009-0-17485-8]

[2] Optimal servicing of geosynchronous satellites [J]. JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2006, 29 (01) : 203 - 206

[3] TIME-, FUEL-, AND ENERGY-OPTIMAL CONTROL OF NONLINEAR NORM-INVARIANT SYSTEMS [J]. IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 1963, : 196 - &

[4] Optimal power-limited rendezvous with upper and lower bounds on thrust [J]. JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1996, 19 (05) : 1124 - 1133

[5] TERMINAL GUIDANCE SYSTEM FOR SATELLITE RENDEZVOUS [J]. JOURNAL OF THE AEROSPACE SCIENCES, 1960, 27 (09): : 653 - &

[6] Fehse W., 2003, Automated Rendezvous and Docking of Spacecraft, P8, DOI [10.1017/CBO9780511543388, DOI 10.1017/CBO9780511543388]

[7] Minimum-Time Trajectory Optimization of Low-Thrust Earth-Orbit Transfers with Eclipsing [J]. JOURNAL OF SPACECRAFT AND ROCKETS, 2016, 53 (02) : 289 - 303

[8] CONTROLLABILITY MINIMUM PRINCIPLE [J]. JOURNAL OF OPTIMIZATION THEORY AND APPLICATIONS, 1975, 17 (1-2) : 93 - 114

[9] Gurfil P, 2016, ASTROPHYS SPACE SC L, V436, P1, DOI 10.1007/978-3-662-50370-6

[10] Nonlinear feedback control of low-thrust orbital transfer in a central gravitational field [J]. ACTA ASTRONAUTICA, 2007, 60 (8-9) : 631 - 648