Residual magnetic dipole cancellation system for satellites

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364459, 244166, B64G 110

Patent

active

050479458

ABSTRACT:
The magnitude and direction of the residual magnetic field or dipole of an orbiting spacecraft is estimated from the attitude-perturbing effects of its interaction with the magnetic field of the heavenly body about which it orbits. The measurements are performed over a significant portion of an orbit. The estimate uses h, the total spacecraft momentum in the body frame, and its body angular rate .omega.. The Earth's magnetic flux density B is determined either by magnetometer measurements, or by recourse to stored historical and ephemeris information.

REFERENCES:
patent: 4084773 (1978-04-01), Schmidt, Jr. et al.
patent: 4114841 (1978-09-01), Muhfelder et al.

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