Fuel-efficient attitude maneuvers of flexible spacecraft with residual vibration reduction into an expected level

Setyamartana Parman; Hideo Koguchi

Setyamartana Parman Bandung Institute of Technology
Hideo Koguchi Nagaoka University of Technology

Abstract

A three-dimensional rest-to-rest attitude maneuver of a satellite with flexible solar panels equipped by on-off reaction jets is studied. Results indicate that, under an unshaped input, the maneuver induces an undesirable motion of the satellite as well as vibration of the solar panels. Fuel-efficient input shapers are then applied to reduce the residual oscillation of its attitude. By reducing vibrations at several large-amplitude natural frequencies, the expected pointing precision of the satellite can be satisfied.

Keywords

References

[1] R.E. Bolz, G.L. Tuve. CRC Handbook of Tables for Applied Engineering Science. CRC Press, Boca Raton, FL, 1973.
[2] H. Hwangbo. The Korea domestic communications and broadcasting satellite system. AIAA, A Collection of Technical Papers of the 14th International Communication Satellite Systems (Washington DC, March 22-24), 1: 550- 555, 1992.
[3] Q. Liu, B. Wie. Robust time-optimal control of uncertain flexible spacecraft. Journal of Guidance, Control, and Dynamics, 15(3): 597- 604, 1992.
[4] L.Y. Pao, W.E. Singhose. A comparison of constant and variable amplitude command shaping techniques for vibration reduction. IEEE Conference on Control Applications (Albany, NY), Institute of Electrical and Electronics Engineers, New York, 875- 881, 1995.
[5] S. Parman, H. Koguchi. Rest-to-rest attitude maneuvers of a satellite with flexible solar panels by using input shapers. Computer Assisted Mechanics and Engineering Sciences, 5(4): 421- 441 , 1998.

Fuel-efficient attitude maneuvers of flexible spacecraft with residual vibration reduction into an expected level

Abstract

Keywords

References

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