论文信息 - Kalman-filtering-based angular velocity estimation using infrared attitude information of spacecraft

Kalman-filtering-based angular velocity estimation using infrared attitude information of spacecraft

We study the problem of estimating the spacecraft attitude angular velocity using the signal of the spacecraft attitude angular sen- sors such as the IR horizon sensor, the star sensor, and the full attitude global positioning systems (GPS) sensor for the first time. A signal state model is established. Based on the linear least mean squares (LMS) error criterion, recursive Kalman filtering is developed for the direct esti- mation of angular velocity. Our algorithm requires relatively few compu- tations and relatively small storage quantities. Finally, the new algorithm is applied to a set of physical simulated IR data, and the results have the advantages of smaller time lag, higher accuracy, and perfect smooth- ness. © 2000 Society of Photo-Optical Instrumentation Engineers. (S0091-3286(00)00702-9)

Yu Shi | Xian-Da Zhang | Xianda Zhang | Yu Shi

[1] Boualem Boashash,et al. Estimating and interpreting the instantaneous frequency of a signal. II. A/lgorithms and applications , 1992, Proc. IEEE.

[2] Susan Rickard,et al. Adaptive neuro-control for spacecraft attitude control , 1995, Neurocomputing.

[3] Rush D. Robinett,et al. NEW PENALTY FUNCTIONS AND OPTIMAL CONTROL FORMULATION FOR SPACECRAFT ATTITUDE CONTROL PROBLEMS , 1997 .

[4] V. P. Makarov,et al. An expert system for design of spacecraft attitude control systems , 1997, Artif. Intell. Eng..

[5] P. Hughes. Spacecraft Attitude Dynamics , 1986 .

[6] Suresh M. Joshi,et al. Robust dissipative compensators for flexible spacecraft control , 1992 .

[7] J. Y. Yang,et al. Robust attitude control of spacecraft using sliding mode control and productive networks , 1997, Int. J. Syst. Sci..

[8] R. German. Sintering theory and practice , 1996 .

[9] Mohinder S. Grewal,et al. Kalman Filtering: Theory and Practice , 1993 .

[10] Y. P. Kakad,et al. Detumbling and reorientation maneuvers and stabilization of NASA SCOLE system , 1992 .

[11] Robert H. Bishop,et al. Adaptive nonlinear control of spacecraft , 1994, Proceedings of 1994 American Control Conference - ACC '94.