Controller for the attitude stabilization of a satellite

Claim 2

In a controller for the attitude stabilization of a satellite, having a first attitude control circuit by means of which said satellite can be returned to a position within predetermined band boundaries, -φ B , +φ B , and having output signals for controlling positive and negative thrust nozzles, the improvement comprising: a second control circuit, said second control circuit being supplied from said first attitude control circuit with values for the attitude angle φ and the angular velocity of the attitude φ, said second control circuit including a comparator means for providing an output signal when φ, φ have the same sign, two AND elements responsive to the output signal of the comparator, two Schmitt triggers responsive to the positive direction and the negative direction of the attitude error respectively, each for supplying an output signal to one of said AND elements, OR elements responsive to the outputs of said AND elements and also responsive to said output signals from the first control circuit, the outputs of said OR elements being used for activating positive and negative thrust nozzles.

Claim 3

A controller according to claim 1, wherein said comparator means provides an output signal when the values φ, φ have reached a predetermined magnitude and sign.

Claim 4

A controller according to claims 1 or 2, wherein said comparator means provides an output signal when the values φ and φ meet the following criteria: 1. |φ|-ω|φ|≧.epsilon., φ>0 upon the occurrence of which the negative thrust nozzle is activated; 2. |φ|-ω|φ|≧.epsilon., φ<0 upon the occurrence of which the positive thrust nozzle is activated wherein ω, ε=constant parameter values.

Claim 5

A controller according to claims 1 or 2, wherein said comparator means has a trigger threshold depending on the values φ and φ, and providing an output signal for controlling said positive and said negative thrust nozzles when the threshold is exceeded.

Claim 6

In a controller for the attitude stabilization of a satellite having first attitude control means for maintaining the attitude of the satellite within predetermined band boundaries, -φ B , +φ B , said control means providing signals representative of the attitude angle of the satellite φ and the angular velocity of attitude φ and also providing uncorrected output signals for controlling positive and negative thrust nozzles, the improvement comprising: second attitude control means for controlling the rate of correction of the attitude of the satellite including: comparator means responsive to the φ and φ signals for providing an output signal when the φ and φ signals have the same sign; first and second trigger means responsive to the φ signal, each for providing an output when its input exceeds a prescribed threshold, said first trigger means responsive to a negative input signal and said second trigger means responsive to a positive input signal; first and second AND elements responsive to output signals from said first and second trigger means respectively and also responsive to the output signal from the comparator means; and first and second OR elements responsive to the outputs of said AND elements respectively and responsive to the uncorrected output signals of the first attitude control means for providing corrected output signals to control the positive and negative thrust nozzles.

Claim 7

In a controller for the attitude stabilization of a satellite having first attitude control means for maintaining the attitude of the satellite within predetermined band boundaries, -φ B , +φ B , said control means providing signals representative of the attitude angle of the satellite φ and the angular velocity of attitude φ and also providing uncorrected output signals for controlling positive and negative thrust nozzles, the improvement comprising: second attitude control means for controlling the rate of correction of the attitude of the satellite including: comparator means responsive to the φ and φ signals for providing an output signal when the φ and φ signals have the same sign; first and second trigger means responsive to the φ signal, each for providing an output when its input exceeds a prescribed threshold, said first trigger means responsive to a negative input signal and said second trigger means responsive to a positive input signal; first and second AND elements responsive to output signals from said first and second trigger means respectively and also responsive to the output signal from the comparator means; and first and second OR elements responsive to the outputs of said AND elements respectively and responsive to the uncorrected output signals of the first attitude control means for providing corrected output signals to control the positive and negative thrust nozzles.