Unloading law for a LEO spacecraft with two-gimbals solar array-Reference-Cited by-同舟云学术

Unloading law for a LEO spacecraft with two-gimbals solar array

Published:2002-12 Issue:12 Volume:51 Page:843-854
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Jan Y.W,Chiou J.C

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference8 articles.

1. Alfriend, K. T. and Lindberg, R. E. Geomagnetic field effects on the design of a magnetic attitude control system. Journal of the Astronautical Science, 1979, XXVII, 269–292.

2. Renard, M. L., Command laws for magnetic attitude control of spin-stabilized Earth satellites. Journal of Spacecraft, 1996, 4(2), 156–163.

3. Wheeler, P. C., Spinning spacecraft attitude control via the environmental magnetic field. Journal of Spacecraft, 1967, 4(12), 1631–1637.

4. Wernli, A., Minimization of reaction wheel momentum storage with magnetic torque. Journal of the Astronautical Sciences, 1978, XXVI(3), 257–278.

5. Stickler, A. C. and Alfriend, K. T., Elementary magnetic attitude control system. Journal of Spacecraft and Rockets, 1976, 13(5), 282–287.

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