DocumentCode :
286662
Title :
Interpolating sliding mode control: an approach to high precision platform control with uncertain dynamics
Author :
Dodds, Stephen J.
Author_Institution :
Dept. of Electr. & Electron. Eng., East London Univ., Dagenham, UK
fYear :
1993
fDate :
34134
Firstpage :
42461
Lastpage :
410
Abstract :
The robustness properties of sliding mode control are exploited in achieving high precision manoeuvring of a space platform to which are attached flexible appendages exhibiting an arbitrary number of flexure modes. Continuous control actuators are assumed. The dynamics parameters are assumed to be unknown but to lie within reasonable practical limits. A new continuous form of discrete-time sliding mode control law is employed. The effects of increasing the iteration interval of the onboard algorithm and errors in the assumed forward path DC gain on the precision with which the platform follows a controlled rate slew demand are investigated. The degree of active flexure mode damping is also investigated
Keywords :
aerospace control; attitude control; discrete time systems; space vehicles; stability; variable structure systems; active flexure mode damping; aerospace control; attitude control; controlled rate slew demand; discrete time systems; flexible appendages; forward path DC gain; robust control; robustness; sliding mode control; space platform; stability; uncertain dynamics; variable structure systems;
fLanguage :
English
Publisher :
iet
Conference_Titel :
High Accuracy Platform Control in Space, IEE Colloquium on
Conference_Location :
London
Type :
conf
Filename :
255868
Link To Document :
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