论文信息 - Stability of Proportional-Plus-Derivative-Plus-Integral Control of Flexible Spacecraft - 字舞流文

Stability of Proportional-Plus-Derivative-Plus-Integral Control of Flexible Spacecraft

P. Hughes | T. Abdel-Rahman

[1] G. T. Tseng,et al. Flexible spacecraft control design using pole allocation technique , 1977 .

[2] Specifying spacecraft flexible appendage rigidity , 1977 .

[3] Vinod J. Modi,et al. Attitude Dynamics of Satellites with Flexible Appendages- A Brief Review , 1974 .

[4] P. C. Hughes,et al. Dynamics of flexible space vehicles with active attitude control , 1974 .

[5] R. Borrelli,et al. An optimization technique for the transient response of passively stable satellites , 1972 .

[6] G. E. Fleischer,et al. Results of flexible spacecraft attitude control studies utilizing hybrid coordinates , 1970 .

[7] P. W. Likins,et al. Dynamics and Control of Flexible Space Vehicles , 1970 .

[8] W. Gevarter. Basic relations for control of flexible vehicles , 1969 .