Multi-valve cooperative control method, device and system for solid vector thruster

A technology of vector thrust and coordinated control, which is applied in the direction of space navigation vehicle guidance device, space navigation vehicle propulsion system device, weight reduction, etc. It can solve the problems of system pressure fluctuation, system structure damage, and uncontrollable combustion of solid propellant.

Pending Publication Date: 2022-08-09
THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD
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Problems solved by technology

However, the combustion of solid propellant cannot be regulated, and the change of each valve of the thruster will cause huge fluctuations in the system pressure, which can easily cause damage to the system structure, excessive deviation of thrust performance, and the system cannot work normally

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  • Multi-valve cooperative control method, device and system for solid vector thruster
  • Multi-valve cooperative control method, device and system for solid vector thruster
  • Multi-valve cooperative control method, device and system for solid vector thruster

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Embodiment Construction

[0071] In order to make the purposes, technical solutions and advantages of the embodiments of the present invention clearer, the technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments These are some embodiments of the present invention, but not all embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without creative work fall within the protection scope of the present invention.

[0072] like figure 1 As shown, an embodiment of the present invention provides a multi-valve cooperative control method for a solid vector thruster, comprising the steps of:

[0073] S100: Establish a linear relationship between the control force required by the pitch, yaw and roll channels and the valve opening degrees of the corresponding...

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Abstract

The invention relates to a solid vector thruster multi-valve cooperative control method, device and system. The solid vector thruster comprises a plurality of thruster valves, the input ends of the multiple thruster valves share a gas generator channel, and output thrust of the multiple thruster valves is used for achieving aircraft attitude control. The control method comprises the following steps: establishing a linear relation between control forces required by pitching, yawing and rolling channels and valve opening degrees of thruster valves corresponding to the channels, and enabling the sum of the valve opening degrees of the plurality of thruster valves to be a fixed value during working; and the output thrust of the corresponding thruster valve is controlled according to the valve opening degree. The multi-valve synergistic effect is achieved while it is guaranteed that the pressure intensity of the system is stable, and vector thrust is continuously adjustable.

Description

technical field [0001] The invention relates to the technical field of solid attitude control power systems, in particular to a multi-valve cooperative control method, device and system for a solid vector thruster. Background technique [0002] The gas generated by solid propellant is used as the working medium, which has the advantages of small size, atmospheric storage, maintenance-free, etc. It has high pressure and large thrust, and can realize the large attitude orbit change of the aircraft under the same space structure mode. However, the combustion of solid propellant cannot be regulated, and the change of each valve of the thruster will cause huge fluctuations in system pressure, which can easily lead to system structure damage, excessive thrust performance deviation, and the system cannot work normally. SUMMARY OF THE INVENTION [0003] The embodiments of the present invention provide a multi-valve cooperative control method, device and system for a solid vector t...

Claims

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Application Information

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IPC IPC(8): B64G1/24B64G1/40
CPCB64G1/244B64G1/402Y02T50/40
Inventor 刘丹赵启扬丁杰王刚周杨梓胡胜云王善金周子翔余明敏原野
Owner THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD
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