A precision closed-loop orbit control device for microsatellites
An orbit control and micro-satellite technology, which is applied in the field of spacecraft orbit control, can solve the problems of reducing the closed-loop control accuracy and failing to provide high-frequency access to accelerometers, and achieves the effect of reducing resource burden and improving orbit control accuracy.
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[0021] The present invention will be further described below in conjunction with the accompanying drawings and specific embodiments.
[0022] The micro-satellite precision orbit control device of the present invention includes an accelerometer meter head and a meter temperature control device, an accelerometer circuit, digital processing circuit hardware, and related software and a calculation unit. The above units are combined into a sealed single-unit device on the star. The accelerometer header and the IF circuit can be replaced by a microsilicon accelerometer.
[0023] (1) Accelerometer header
[0024] The accelerometer head is a quartz flexible accelerometer. The meter head needs temperature control, and the temperature control should close the meter head and implement temperature control. The temperature control accuracy is ±0.2°C. This is the second-level temperature control, and the temperature control accuracy of the first-level temperature control (at the overall ...
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Abstract
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