An attitude control sysytem design based on the TURKSAT-1B geostationary satellite

Date

1997-12-17

Author

Tekinalp, Ozan
Tulunay, Yurdanur

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Attitude control algorithms for a geostationary satellite which employs a strap down momentum wheel gyro for pitch control and thrusters for roll control is developed. Pitch control is realised using a ladder network type Schmitt triggers with hysteresis and a feedback lag circuit. An effectiveness of the design is demonstrated. Roll control law uses thruster on/off control scheme. The effect of thruster pulse amplitude and pulse duration on fuel consumption is investigated, and a proper pair are given.

URI

https://hdl.handle.net/11511/52673

Collections

Department of Aerospace Engineering, Conference / Seminar

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Citation Formats

O. Tekinalp and Y. Tulunay, “An attitude control sysytem design based on the TURKSAT-1B geostationary satellite,” 1997, vol. 10, Accessed: 00, 2020. [Online]. Available: https://hdl.handle.net/11511/52673.