Airplane longitudinal gravity center deploying control method
A control method and center of gravity technology, applied in electric controllers, aircraft component testing, controllers with specific characteristics, etc., can solve problems such as poor stability, poor real-time performance, and low deployment accuracy, so as to improve accuracy and real-time performance , the effect of speeding up the deployment process
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[0026] The technical solutions in the embodiments of the present invention will be clearly and completely described below in conjunction with the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.
[0027] The invention provides an aircraft vertical center of gravity allocation control method. The system achieves the goal of changing the aircraft center of gravity by allocating the water volume in different water tanks, specifically by controlling the closure of the water outlet valve of the water tank, the switch of the pump, and the opening of the electric ball valve. The allocation of water volume, and then realize the precise allocation of the center of ...
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