Patent ID: 6024327
Filing Date: 2000-02-15
Classification: B64G

Abstract:
An intelligent control apparatus for a satellite, comprising:an orbit and attitude determining and predicting means for determining and predicting orbit and attitude of a satellite according to a plurality of orbit sensor data;a control judging means for judging the orbit and the attitude according to the orbit data and the attitude data determined and predicted by said orbit and attitude determining and predicting means;an anomaly control judging means for judging whether an anomaly control executes according to a plurality of anomaly sensor data;a control parameter computing means for computing orbit and attitude control parameters by using an optimal control method according to the result of judgment of said control judging means, or computing anomaly control parameters by using the optimal control method according to the result of judging of said anomaly control judging means;a control command generating means for generating orbit and attitude control commands according to orbit and attitude parameters computed by said control parameter computing means, or generating anomaly control commands according to anomaly control parameters computed by said control parameter computing means; and,a control command processing means for processing orbit and attitude commands or anomaly control commands generated from said control command generating means.