应用旋转矩阵的卫星姿态输出反馈机动控制

doi:10.7527/S1000-6893.2016.0114

Abstract

Abstract:

An output-feedback attitude maneuver control strategy in the absence of angular velocity feedback is proposed for rigid satellite system by solely and directly using unit-length vector measurements. The orientation of a rigid body is described by a rotation matrix directly, rather than by a parameterization, avoiding the undesirable singular problem and unwinding phenomenon caused by Euler angle, quaternion or the modified Rodrigues parameters (MRPs) representations of the attitude. A new orientation error of the rigid body is computed by the vector measurements and a set of desired vector measurements. By using the lead filter, the velocity-free attitude maneuver control law that ensures set-point regulation is developed. Within the Lyapunov framework, the global stability of the close-loop system is guaranteed. Numerical simulation results demonstrate the successful set-point regulation of the proposed output-feedback control strategy.

Key words: rigid satellite, attitude maneuver, rotation matrix, output feedback, vector measurements

CLC Number:

V442.8

HUANG Jing, LIU Gang, LIU Fucheng, LI Chuanjiang. Output feedback attitude maneuver control of satellite using rotation matrix[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016, 37(12): 3774-3782.

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Output feedback attitude maneuver control of satellite using rotation matrix

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