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- W1567630282 abstract "Control problem of a spacecraft is an important topic in automatic control engineering. A body orbiting the Earth in geosynchronous orbit has instabilities in attitude dynamics and disturbances caused by the Earth, the Moon, the Sun and other bodies in space. These effects force the body to lose initial orbit and attitude. Here the control system takes important part of spacecraft missions where it keeps the body in designed orbit and desired attitude. The control system consists of control elements and control algorithms which are developed for the mission by a control engineer [1]. The commonly used control elements for a spacecraft in geosynchronous orbit are thrusters, reaction or momentum wheels, etc." @default.
- W1567630282 created "2016-06-24" @default.
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- W1567630282 date "2012-03-23" @default.
- W1567630282 modified "2023-10-01" @default.
- W1567630282 title "Design of Sliding Mode Attitude Control for Communication Spacecraft" @default.
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- W1567630282 doi "https://doi.org/10.5772/38114" @default.
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