Planning algorithm for multiple satellite clusters

被引:68
作者
Campbell, ME [1 ]
机构
[1] Cornell Univ, Dept Mech & Aerosp Engn, Ithaca, NY 14853 USA
关键词
D O I
10.2514/2.5111
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
A generalized planning methodology for satellite clusters is proposed. The methodology utilizes Hamilton-Jacobi-Bellman optimality (minimum time or minimum fuel) to generate quickly a set of maneuvers from an initial stable formation to a final stable formation. Maneuvers are selected from the original set based on the maneuver time, fuel, and collision proximity. The final maneuvers are calculated by optimizing the switch times using a realistic set of orbital dynamics. The algorithm is developed to be distributed and scales well as the number of satellites increases. A minimal level of communication is used because only switch times and collision proximity information are distributed from the planner. An example with four satellites maneuvering in an eccentric orbit (e = 0.2) is presented. Results show that optimal cluster maneuvers (minimum time or minimum fuel) can be generated within minutes, and most of the computational implementation can be accomplished in parallel.
引用
收藏
页码:770 / 780
页数:11
相关论文
共 28 条
[1]  
BRYSON A, 1994, CONTROL SPACECRAFT A, P103
[2]  
CAMPBELL M, 2002, 2002 AM CONTR C I EL, P1686
[3]  
CAPPS RW, 1996, JPL PUBL, V9621
[4]   Decentralized control of satellite formations [J].
Carpenter, JR .
INTERNATIONAL JOURNAL OF ROBUST AND NONLINEAR CONTROL, 2002, 12 (2-3) :141-161
[5]   FUEL-OPTIMAL RENDEZVOUS NEAR A POINT IN GENERAL KEPLERIAN ORBIT [J].
CARTER, T ;
HUMI, M .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1987, 10 (06) :567-573
[6]   State transition matrices for terminal rendezvous studies: Brief survey and new example [J].
Carter, TE .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1998, 21 (01) :148-155
[7]  
CORAZZINI T, 1998, J I NAVIGATION, V45, P195
[8]  
DAS A, 1998, 985255 AIAA, P1
[9]   Relative dynamics and control of spacecraft formations in eccentric orbits [J].
Inalhan, G ;
Tillerson, M ;
How, JP .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2002, 25 (01) :48-59
[10]  
Kirk D. E., 1970, OPTIMAL CONTROL THEO, P240