Design of the Suboptimal Profiled Relay Control of Orientation of the Spacecraft Having Elastic Structural Elements with Regard for Two Oscillation Tones

被引：0

作者：

A. S. Buryi

Yu. I. Krylov

S. V. Matsykin

机构：

[1] Peter the Great Military Academy of Strategic Rocket Forces,

来源：

Automation and Remote Control | 2002年 / 63卷

关键词：

Mechanical Engineer; System Theory; Oscillation Amplitude; Spacecraft Motion; Relay Control;

D O I：

暂无

中图分类号：

学科分类号：

摘要：

A speed-optimal formulation of the control of angular spacecraft motion with regard for two tones of oscillations of its elastic structural elements was considered. A new approach based on the relay profiling of control was proposed. It provides the minimum oscillation amplitudes of the tones under consideration.

引用

页码：550 / 559

页数：9

共 4 条

[1] Design of the suboptimal profiled relay control of orientation of the spacecraft having elastic structural elements with regard for two oscillation tones
Buryi, AS
Krylov, YI
Matsykin, SV
AUTOMATION AND REMOTE CONTROL, 2002, 63 (04) : 550 - 559
[2] Design of suboptimal relay contouring orientation control for a spacecraft with elastically strained construction elements with account for combinations of two types
Buryj, A.S.
Krylov, Yu.I.
Matsykin, S.V.
2002, Nauka, Moscow
[3] Two-level orientation control system of flexible spacecraft with active stabilization of structural elastic oscillations
Ermilov, A. S.
Ermilova, T. V.
Rutkovskii, V. Yu.
Sukhanov, V. M.
AUTOMATION AND REMOTE CONTROL, 2008, 69 (06) : 929 - 941
[4] Two-level orientation control system of flexible spacecraft with active stabilization of structural elastic oscillations
A. S. Ermilov
T. V. Ermilova
V. Yu. Rutkovskii
V. M. Sukhanov
Automation and Remote Control, 2008, 69 : 929 - 941

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