FIELD: physics.
SUBSTANCE: autopilot system has a two-channel circuit for processing the input signal of the autopilot system and identical 1st and 2nd channels respectively having 1st and 2nd phase detectors, 1st and 2nd low-pass filters, 1st and 2nd adders, 1st and 2nd modulators and a 3rd adder. The output of the 1st modulator is connected to the first input of the 3rd adder and the output of the 2nd modulator is connected to the second input of the 3rd adder whose output is the output of the autopilot system. The autopilot also has 3rd and 4th phase detectors whose data inputs are connected and form the second data input of the autopilot system. There also 1st, 2nd, 3rd and 4th circuits for selecting the period average carrier input signal, 3rd and 4th low-pass filters, 1st and 2nd functional units and 1st and 2nd limiters. The gain control channel consists of series-connected adder, square-rooting circuit and non-linearity unit.
EFFECT: accuracy of generated autopilot control signal for a spin rocket with single-channel control with variation of its rotation frequency.
2 dwg
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Authors
Dates
2010-09-27—Published
2008-09-12—Filed