论文信息 - DESIGN AND GLOBAL ANALYSIS OF SPACECRAFT ATTITUDE CONTROL SYSTEMS - 字舞流文

DESIGN AND GLOBAL ANALYSIS OF SPACECRAFT ATTITUDE CONTROL SYSTEMS

Mathematical model of global spacecraft attitude control system based on three dimensional motion

G. Meyer | G. Meyer

[1] G. Meyer,et al. On the use of Euler's theorem on rotations for the synthesis of attitude control systems , 1966 .

[2] R. Showman. Simplified processing of star tracker commands for satellite attitude control , 1967, IEEE Transactions on Automatic Control.

[3] G. Meyer. Response envelope - A global description of three-axis large angle spacecraft attitude control systems , 1968 .

[4] G. Meyer. On the use of orthogonal transformation for the synthesis of attitude control systems. , 1966 .

[5] L. S. Pontryagin,et al. Mathematical Theory of Optimal Processes , 1962 .

[6] F. J. Moran,et al. Air bearing table mechanization and verification of a spacecraft wide angle attitude control system. , 1970 .

[7] Q. M. Hansen,et al. A gyroless solar pointing attitude control system for the Aerobee sounding rocket. , 1967 .

[8] G. Meyer. The design of a large angle three-axis attitude servomechanism for spacecraft , 1967 .