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Method and apparatus for simulating large thruster on spacecraft

A thruster and spacecraft technology, applied in the field of simulation verification, can solve difficult problems such as large-scale thruster simulation verification, and achieve the effect of fewer components, lower costs, and less demanding components

Inactive Publication Date: 2010-09-29
HARBIN INST OF TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] At present, in the full physical simulation of spacecraft based on the air-floating three-axis turntable, due to the limitation of the simulation environment and cost, the simulation of the spacecraft actuator generally only considers the flywheel, and it is difficult to realize the simulation verification of all large thrusters on the spacecraft.

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  • Method and apparatus for simulating large thruster on spacecraft
  • Method and apparatus for simulating large thruster on spacecraft
  • Method and apparatus for simulating large thruster on spacecraft

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Embodiment Construction

[0024] The present invention will be further described below in conjunction with accompanying drawing and specific embodiment:

[0025] In this embodiment, six groups of thrusters are respectively installed in the roll direction, pitch direction and yaw direction of the air-floating three-axis turntable. After measuring the moment of inertia of the turntable, according to the design principle of equivalent scaling, the size of the equivalent control torque required on the turntable is obtained. Simulation verification of the working state of large thrusters during orbital flight.

[0026] to combine figure 1 , the present invention includes small thrusters installed on the three-axis air-floating turntable, 6 sets of thrusters are installed around the three-axis air-floating turntable, and the thruster groups A1 / B1 and A2 / B2 are installed on the positive side of the X-axis in the OXY plane In the positive and negative directions, thrust is generated to form the moment in the...

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Abstract

The invention provides a method of a large-scale thrustor on a simulation spacecraft and a device thereof. The invention uses an air flotation three-axle table to simulate the body of a spacecraft. A control moment is formed by the push power generated by a plurality of small scale thrustors installed in different directions of the air flotation three-axle table. When the three-axle table works, namely when the spacecraft operates in orbit, the push power generated by small scale nozzles in all directions of the table drives the spacecraft to a target position according to a control instruction. In virtue of the design principle of equivalent scaling, the simulation of the control function of a large scale thrustor on a real spacecraft can be realized. The method is applicable to all situations that the air flotation tables are used for simulating the operation of the spacecraft in orbit and can lower the cost of ground simulation verification of the thrustor technology on the spacecraft.

Description

(1) Technical field [0001] The invention relates to a simulation verification method, in particular to a technology for simulating all large thrusters on a spacecraft. (2) Background technology [0002] The full physical simulation of the satellite control system is a unique simulation method in the process of satellite development. It uses the air-floating three-axis turntable as a motion simulator, also known as air-floating table simulation. The full physical simulation of the satellite control system uses the air-floating three-axis turntable to simulate the satellite body as the control object, and the control system uses the satellite control system for simulation. When a space vehicle performs a full-physics simulation, it is necessary to simulate important space environments such as weightlessness or no resistance on the ground. [0003] The air-floating three-axis turntable uses compressed air to form an air film between the air-floating bearing and the bearing sea...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G09B25/00
Inventor 陈雪芹王峰耿云海兰盛昌叶东杨正贤董晓光
Owner HARBIN INST OF TECH