Input-to-State Stable Attitude Control

被引:14
|
作者
Hokayem, Peter F. [1 ]
Schilling, Klaus [1 ]
机构
[1] Univ Wurzburg, D-97074 Wurzburg, Germany
关键词
D O I
10.2514/1.37529
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Simulation about Proportional-plus-Derivative (PD)-type control laws which are not generally robust as regards to bounded disturbances and provide a sufficient condition for nonlinear type control laws to render system semiglobally input-to-state-stable (ISS) was proposed. The main concept of ISS is to characterize the stability of system under bounded disturbances. The Clayey-Rodriguez parameterization suffered from lack of robustness with respect to bounded disturbances from simple PD type attitude control. A nonlinear control law was proposed with sufficient condition under which the closed-loop system was semiglobally ISS. Hence, it was constructed in a way that any given restriction on the initial state and disturbance input, for large design control gains that can render the system input-to-state stable within the stated restrictions.
引用
收藏
页码:1826 / 1829
页数:4
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