GENERATION OF THE RAMMED CONTROL BY GYRO ACTUATORS OF THE SPACECRAFT CONTROL SYSTEM IN THE ATTITUDE-CHANGE MODE

机译：姿态变化模式下空间控制系统的陀螺执行器的RAMRAM控制的产生

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摘要

A new approach to the problem of constructing the program control of attitude-varying of spacecraft with gyroactua-tors is considered. This approach uses the property of controllability of assigned states of the dynamic object, whose model is described by nonlinear ordinary differential equations. For the purpose of solving the controllability problem of the nonlinear system, a new method of solving nonlinear two-point boundary-value problems for controlled systems is applied.

机译：提出了一种构造具有陀螺致动器的航天器姿态变化程序控制问题的新方法。这种方法利用了动态对象分配状态的可控制性，该对象的模型由非线性常微分方程描述。为了解决非线性系统的可控制性问题，应用了一种解决受控系统的非线性两点边值问题的新方法。

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来源
《Saint Petersburg International Conference on Integrated Navigation Systems; 20040524-26; Saint Petersburg(RU)》|2004年|P.291-293|共3页
会议地点 Saint Petersburg(RU)
作者
S.N. Vassilyev; V.A.Voronbv; E.I. Druzhinin;
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作者单位

Institute of System Dynamics and Control Theory of SB RAS 134, Lermontov St., 664033, Irkutsk;

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会议组织
原文格式 PDF
正文语种 eng
中图分类无线电导航;
关键词
controllability; program control; spacecraft; gyrodynes;

机译：可控性;程序控制;航天器;陀螺;

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GENERATION OF THE RAMMED CONTROL BY GYRO ACTUATORS OF THE SPACECRAFT CONTROL SYSTEM IN THE ATTITUDE-CHANGE MODE

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