제어로봇시스템학회:학술대회논문집
- 1995.10a
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- Pages.444-447
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- 1995
Average performance of risk-sensitive controlled orbiting satellite and three-degree-of-freedom structure
- Won, Chang-Hee (TT& C Section, Satellite Communications Technology Division, Electronics and Telecommunications Research Institute (ETRI))
- Published : 1995.10.01
Abstract
The satellite in a circular orbit about a planet with disturbances and a three-degree-of-freedom (3DOF) structure under seismic excitations are modeled by the linear stochastic differential equations. Then the risk-sensitive optimal control method is applied to those equations. The mean and the variance of the cost function varies with respect to the risk-sensitivity parameter, .gamma.