论文信息 - Methods and Software for Nonlinear Dynamic Research of Spacecraft Fault Tolerant Control Systems

Methods and Software for Nonlinear Dynamic Research of Spacecraft Fault Tolerant Control Systems

Abstract New results on methods and software for nonlinear dynamic research and design of the precise gyromoment fault tolereant control systems by the information spacecraft (remote sensing, communication, navigation and geodetic) developed by the leading Russian State Space Research and Production Associations (RPAs) — the TsSKB -Progress and the NPO PM , are presented.

Ye.I. Somov | G. P. Anshakov | V. P. Makarov | V. A. Rayevsky | A. G. Kozlov

[1] Paul M. Frank,et al. Fault diagnosis in dynamic systems using analytical and knowledge-based redundancy: A survey and some new results , 1990, Autom..

[2] John L. Junkins,et al. Feedback Control Law for Variable Speed Control Moment Gyros , 1998 .

[3] Costas Kravaris,et al. System-theoretic properties of sampled-data representations of nonlinear systems obtained via Taylor-Lie series , 1997 .

[4] O. A. Kondrat'yev,et al. Ultra-precision attitude control of a large low-orbital space telescope , 1999 .

[5] J. W. Crenshaw. 2-SPEED, a single-gimbal control moment gyro attitude control system. , 1973 .

[6] P. Frank. Enhancement of robustness in observer-based fault detection† , 1994 .