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Gravity center allocation control method based on liquid level monitoring of single water tank

A control method and liquid level monitoring technology, which is applied in the direction of aircraft component testing, etc., can solve the problems of uneven water inlet and outlet speeds and unsymmetrical design of the system, etc.

Active Publication Date: 2021-05-28
HARBIN INST OF TECH +2
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  • Description
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  • Application Information

AI Technical Summary

Problems solved by technology

Although the deployment process involves the participation of all water tanks, due to the limited layout area of ​​the system, the system cannot be designed completely symmetrically
In addition, there is an attitude angle during the flight of the aircraft. These factors lead to uneven water inlet and outlet speeds of each water tank when the center of gravity is adjusted.

Method used

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  • Gravity center allocation control method based on liquid level monitoring of single water tank
  • Gravity center allocation control method based on liquid level monitoring of single water tank
  • Gravity center allocation control method based on liquid level monitoring of single water tank

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Embodiment Construction

[0030] 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.

[0031] The present invention provides an aircraft longitudinal center of gravity allocation control method based on the liquid level monitoring of a single water tank. The system monitors the liquid level of each water tank and adjusts the water volume in each water tank according to the allocation method, so as to obtain the goal of adjusting the center of gravity of the aircraft. Specifically, the allocation of different water volumes is realized by controlling...

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Abstract

The invention discloses a gravity center allocation control method based on liquid level monitoring of a single water tank, and belongs to the technical field of gravity center allocation control in an aircraft test flight test. The control method comprises the following steps: 1, setting a torque threshold capable of starting adjustment; and 2, calculating a moment amount required to be changed for reaching the target gravity center, judging whether the moment amount is greater than a threshold value of the moment amount capable of starting adjustment or not, and monitoring whether the liquid level of a single water tank reaches an alarm value or not in real time, so as to start a water pump and control the opening degree of an electric ball valve to complete the allocation of the gravity center. The method is designed based on the FPGA, the real-time performance and the accuracy of the control method are improved by utilizing the rapid parallelism of the FPGA, the liquid level of each water tank is monitored, all the water tanks are transferred to participate in gravity center allocation, the liquid level distribution of the water inlet and outlet water tanks is adjusted according to the liquid level monitoring of the single water tank, and the control method combining feedforward and PID is adopted, and meanwhile, a pre-closing strategy is combined to efficiently complete center-of-gravity deployment.

Description

technical field [0001] The invention relates to a center-of-gravity allocation control method based on liquid level monitoring of a single water tank, and belongs to the technical field of center-of-gravity allocation control in aircraft flight tests. Background technique [0002] In the process of aircraft development and flight test, the center of gravity envelope detection is one of the most important indicators, which directly affects the flight safety of the aircraft. The center of gravity adjustment system is an automatic adjustment device based on water medium, which has been widely used by international civil aviation airliner companies. The center of gravity adjustment system can realize rapid and accurate adjustment of the center of gravity during the test flight process related to the center of gravity of the aircraft, realize the functions of maintaining the center of gravity of the aircraft center of gravity in different flight stages, and effectively improve th...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64F5/60
CPCB64F5/60
Inventor 魏德宝乔立岩孙科徐敦闫宏亮彭喜元杨春霞
Owner HARBIN INST OF TECH