| 航天飞行器控制系统误差实时补偿方案研究 |
| |
| 引用本文： | 王永平.航天飞行器控制系统误差实时补偿方案研究[J].航天控制,1995(2). |
| |
| 作者姓名： | 王永平 |
| |
| 作者单位： | 北京航天自动控制研究所 |
| |
| 摘 要： | 箭上计算机实时计算因惯性器件系统误差而造成的测速误差，并将其引入导航方程后，通过导引和关机进行实时补偿。数学仿真表明采用这种补偿方案，箭载计算机的计算工作量小，补偿精度高，是一种有实用价值的方案。
|
| 关 键 词： | 航天器控制系统，误差，补偿 |
Research on Real-Time Error Compensation for Aerospace Vehicle Control System |
| |
| Wang Yongping.Research on Real-Time Error Compensation for Aerospace Vehicle Control System[J].Aerospace Control,1995(2). |
| |
| Authors: | Wang Yongping |
| |
| Institution: | Beijing Aerospace Automatic Control institute 100854 |
| |
| Abstract: | The on-board computer computes at real-time the velocity measurement errors created by the inertial device system errors and leads the errors into the navigation equation. Afler that, real-time compensation is carried on through steering and cutoff The mathematical simulation shows that afler adopting this compensation concept, computation amount of the on-board computer is small and compensation accuracy is high. This compensation concept is of practical value. |
| |
| Keywords: | terms Spacecraft control system Error Compensation |
| 本文献已被 CNKI 等数据库收录！ |
