RESTRAINED VARIABLE STRVCTURE CONTROL FOR A CLASS OF FLEXIBLE SATELLITE

LIU Chunmei; SHEN Yi; HU Hengzhang

doi:10.11728/cjss2000.01.081

Volume 20 Issue 1

Jan. 2000

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Article Navigation > Chinese Journal of Space Science > 2000 > 20(1): 81-88

LIU Chunmei, SHEN Yi, HU Hengzhang. RESTRAINED VARIABLE STRVCTURE CONTROL FOR A CLASS OF FLEXIBLE SATELLITE[J]. Chinese Journal of Space Science, 2000, 20(1): 81-88. doi: 10.11728/cjss2000.01.081

Citation:

LIU Chunmei, SHEN Yi, HU Hengzhang. RESTRAINED VARIABLE STRVCTURE CONTROL FOR A CLASS OF FLEXIBLE SATELLITE[J]. Chinese Journal of Space Science, 2000, 20(1): 81-88. doi: 10.11728/cjss2000.01.081

LIU Chunmei, SHEN Yi, HU Hengzhang. RESTRAINED VARIABLE STRVCTURE CONTROL FOR A CLASS OF FLEXIBLE SATELLITE[J]. Chinese Journal of Space Science, 2000, 20(1): 81-88. doi: 10.11728/cjss2000.01.081

Citation:

LIU Chunmei, SHEN Yi, HU Hengzhang. RESTRAINED VARIABLE STRVCTURE CONTROL FOR A CLASS OF FLEXIBLE SATELLITE[J]. Chinese Journal of Space Science, 2000, 20(1): 81-88. doi: 10.11728/cjss2000.01.081

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RESTRAINED VARIABLE STRVCTURE CONTROL FOR A CLASS OF FLEXIBLE SATELLITE

doi: 10.11728/cjss2000.01.081 cstr: 32142.14.cjss2000.01.081

Department of Control Engineering, Harbin institute of Technology 150001

Received Date: 1999-02-05
Rev Recd Date: 1999-07-28
Publish Date: 2000-01-24

Abstract

Abstract

In this paper, a new method for the attitude control of a class of flexible satelliteunder restrained control is presented. The target of the variable structure systemis changed step by step according to the bounded control, which makes the controlinputs under the bound of the execution. Thereby a equivalent unbounded variablestructure control system comes into being which satisfies the reaching condition ofsliding mode.
- Satellite,
- Flexible,
- Variable structure control