A de-orbit method for geostationary communication satellites
A geostationary orbit, communication satellite technology, applied in the direction of artificial satellites, space navigation equipment, space navigation aircraft, etc., can solve the problem of inaccurate estimation of the remaining propellant, inability to complete deorbit, unsuccessful deorbit, etc. , to facilitate the adjustment of the control strategy, ensure the visible measurement and control time of the cruise, and achieve the effect of small impact
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[0051] The present invention will be described in detail below with reference to the accompanying drawings and embodiments.
[0052] A de-orbit method for geostationary orbit communication satellites is mainly divided into three parts: de-orbit maneuver control method; propellant emptying; satellite passivation method. Follow the following principles: safe and controllable; batch and reasonable iteration; easy to operate.
[0053] Specific steps are as follows:
[0054] Step 1. Satellite health check and status setting: a) Conduct a comprehensive health check on the satellite control sub-system, power sub-system, measurement and control sub-system, propulsion sub-system, transponder sub-system, etc. to confirm the normal working status; Sensitive measurement equipment such as solar sensor, star sensor and other sensitive measurement equipment to carry out health inspection; b) Status setting: calibrate the thruster, determine the ignition pulse width and period; test and cont...
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