Multiple Model Adaptive Attitude Control of LEO Satellite with Angular Velocity Constraints

다국어 초록 (Multilingual Abstract)

In this paper, the multiple model adaptive control is utilized to improve the transient response of attitude control system for a rigid spacecraft. An adaptive output feedback control law is proposed for attitude control under angular velocity constraints and its almost global asymptotic stability is proved. The multiple model adaptive control approach is employed to counteract large uncertainty in parameter space of the inertia matrix. The nonlinear dynamics of a low earth orbit satellite is simulated and the proposed control algorithm is implemented. The reported results show the effectiveness of the suggested scheme.

참고문헌 (Reference)

1 Tayebi A, "Unit quaternion-based output feedback for the attitude tracking problem" 53 (53): 1516-1520, 2008

2 Wen JT-Y, "The attitude control problem" 36 (36): 1148-1162, 1991

3 Zhang W, "Stable weighted multiple model adaptive control: discrete-time stochastic plant" 27 (27): 562-581, 2013

4 Tsiotras P, "Stabilization and optimality results for the attitude control problem" 19 (19): 772-779, 1996

5 Hassani V, "Stability analysis of robust multiple model adaptive control" 44 (44): 350-355, 2011

6 Sidi MJ, "Spacecraft dynamics and control: a practical engineering approach. Cambridge aerospace series" Cambridge University Press 1997

7 Wertz JR, "Spacecraft attitude determination and control, vol 73" Springer 1978

8 Singh S, "Robust nonlinear attitude control of flexible spacecraft" AES-23 (AES-23): 380-387, 1987

9 Capua A, "Robust nonlinear $H{\infty}$ output-feedback for spacecraft attitude control" 2014

10 Hu Q, "Robust attitude control design for spacecraft under assigned velocity and control constraints" 52 (52): 480-493, 2013

11 Chaturvedi N, "Rigid-body attitude control" 31 (31): 30-51, 2011

12 Wie B, "Quaternion feedback for spacecraft large angle maneuvers" 8 (8): 360-365, 1985

13 Lu Jianbo, "Nonlinear quaternion feedback control for spacecraft via angular velocity shaping" 1 : 632-636, 1994

14 Han Z, "Newconcepts in adaptive control using multiple models" 57 (57): 78-89, 2012

15 Maybeck PS, "Multiple model adaptive algorithms for detecting and compensating sensor and actuator/surface failures in aircraft flight control systems" 9 (9): 1051-1070, 1999

16 Fekri S, "Issues, progress and new results in robust adaptive control" 20 (20): 519-579, 2006

17 Ngo KB, "Integrator backstepping design for motion systems with velocity constraint" 141-146, 2004

18 Seo D, "High-performance spacecraft adaptive attitude-tracking control through attracting-manifold design" 31 (31): 884-891, 2008

19 Tsiotras P, "Further passivity results for the attitude control problem" 43 (43): 1597-1600, 1998

20 Markley FL, "Fundamentals of spacecraft attitude determination and control" Springer 2014

21 Zou A-M, "Finite-time output feedback attitude tracking control for rigid spacecraft" 22 (22): 338-345, 2014

22 Lizarralde F, "Attitude controlwithout angular velocity measurement: a passivity approach" 41 (41): 468-472, 1996

23 Schaub H, "Analytical mechanics of space systems" American Institute of Aeronautics and Astronautics Inc 2014

24 Singla P, "An adaptive attitude control formulation under angular velocity constraints" 2008

25 Show L-L, "An LMI-based nonlinear attitude control approach" 11 (11): 73-83, 2003

26 Singla P, "Adaptive output feedback control for spacecraft rendezvous and docking under measurement uncertainty" 29 (29): 892-902, 2006

27 Guo Y, "Adaptive finite-time backstepping control for attitude tracking of spacecraft based on rotation matrix" 27 (27): 375-382, 2014

28 Narendra KS, "Adaptive control using multiple models" 42 (42): 171-187, 1997

29 Schaub H, "Adaptive control of nonlinear attitude motions realizing linear closed loop dynamics" 24 (24): 95-100, 2001

30 Lu K, "Adaptive attitude tracking control for rigid spacecraft with finite-time convergence" 49 (49): 3591-3599, 2013

31 Bhat SP, "A topological obstruction to continuous global stabilization of rotational motion and the unwinding phenomenon" 39 (39): 63-70, 2000

32 Salcudean S, "A globally convergent angular velocity observer for rigid body motion" 36 (36): 1493-1497, 1991