High-precision control of the observation satellite with small power consumption

被引：0
|
作者：
Meshchanov A.S. [1 ]
机构：
[1] Tupolev State Technical University, Kazan
来源：
Russian Aeronautics (Iz VUZ) | 2008年 / 51卷 / 1期
基金：
俄罗斯基础研究基金会;
关键词：
Power Consumption; Observation Satellite; Sliding Mode; RUSSIAN Aeronautic; Terminal Position;
D O I：
10.3103/S1068799808010042
中图分类号：
学科分类号：
摘要：
An unified method of the control, orientation and stabilization is proposed; the method allows an observation satellite (OS) to be brought in the sliding mode with a specified accuracy and in a required time to the necessary angular terminal position in the conditions of the limited indefinite external disturbances. The method minimizes power consumption for control. An approach for regulation of the frequency and amplitude of steady-state control oscillations is presented. © Allerton Press, Inc. 2008.
引用
收藏
页码：16 / 25
页数：9
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