제어로봇시스템학회:학술대회논문집
- 1993.10a
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- Pages.799-804
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- 1993
A station-keeping method considering satellite attitude
자세를 고려한 위성체 궤도유지 기법
Abstract
In this paper, the scheme of combining the orbit correction and attitude control of a 3-axis stabilized satellite is suggested. Being coupled and complimentary, it is preferable to achieve the required orbit correction and the desired attitude control simultaneously. A solution of the probes simultaneous control of orbit correction and attitude of a satellite, is obtained by solving the two point boundary value problem numerically. The first-order gradient algorithm is used to solve the numerical problem. The simulation results show that the East-West station keeping process with the combined system of an orbit correction and an attitude control is satisfactory.
Keywords