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Three-axis air-bearing table guide method for verifying satellites formation

A satellite formation and air-floating platform technology, which is applied in the field of three-axis air-floating platform guidance, can solve the problems of complex coordination of multiple simulated satellites, and achieve the effect of easy implementation and wide application range.

Inactive Publication Date: 2010-10-06
HARBIN INST OF TECH
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  • Summary
  • Abstract
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  • Claims
  • Application Information

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Problems solved by technology

[0006] The purpose of the present invention is to solve the problem of complex coordination among multiple simulated satellites, and to provide a three-axis air bearing platform guidance method for verifying satellite formation

Method used

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  • Three-axis air-bearing table guide method for verifying satellites formation
  • Three-axis air-bearing table guide method for verifying satellites formation
  • Three-axis air-bearing table guide method for verifying satellites formation

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specific Embodiment approach 1

[0022] Specific implementation mode one: the following combination figure 1 and figure 2 This embodiment will be specifically described. A three-axis air-floating platform guidance method for verifying satellite formation, said method is based on a simulation platform including three three-axis air-floating platforms, respectively using three three-axis air-floating platforms as three simulated satellites, the simulation platform The console controls the movement of the three-axis air bearing table,

[0023] Applying the simulation platform to verify the guidance method of the three-axis air bearing platform of the satellite formation is as follows:

[0024] Step 1. Set the three simulated satellites as the main satellite, the first slave satellite and the second slave satellite respectively, and determine the movement mode of each simulated satellite;

[0025] Step 2. According to the motion pattern of each simulated satellite, the console pre-sets the motion trajectory p...

specific Embodiment approach 2

[0037] Specific embodiment 2: This embodiment is a further limitation of the three-axis air bearing platform guidance method for verifying the satellite formation described in the specific embodiment 1. In step 1, the movement patterns of each simulated satellite described in detail It means: the master star rotates at the set position, the first slave star and the second slave star take the position of the master star as the center, and fly in a counterclockwise movement mode.

[0038] According to the mission requirements and implementation methods of formation flight, there are many models of satellite formation, and the leader-follower model is adopted in this embodiment. In formation flight missions, one simulated satellite is established as the master star, and the rest of the simulated satellites are set as slave stars.

specific Embodiment approach 3

[0039]Specific embodiment three: This embodiment is a further limitation of the three-axis air bearing platform guidance method for verifying satellite formation described in specific embodiment one, and the trajectory parameters of each simulated satellite described in step two refer to , the position of the master star, the center and radius of the trajectory of the first slave star, and the center and radius of the trajectory of the second slave star.

[0040] The movement trajectory of the slave star relative to the master star described in this embodiment is called the movement trajectory of the slave star, and the different forms of the movement trajectory of the slave star form various formation configurations.

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Abstract

The invention relates to a three-axis air-bearing table guide method for verifying a satellite formation, which solves the problem of complex coordination among multiple analogue satellites. The guide method is implemented on the basis of a simulation platform having three three-axis air-bearing tables and comprises: 1, determining the functions and motion modes of the analogue satellites; 2, planning the motion trails of the analogue satellites; 3, measuring the data of the analogue satellites in real time and guiding a first following satellite and a second following satellite respectively; 3.1, determining the motion destinations of the following satellites to be guided; 3.2, calculating the distances between the following satellites to be guided and current motion destinations in real time; 3.3, judging if the distances are smaller than offset values allowed by a system; 3.4 judging if the flight task is finished; 3.5, adjusting the motion directions of the following satellites to be guided; and 3.6, determining next motion destinations of the satellites to be guided. The method realizes the three-axis air-bearing table guidance of the satellite formation and is applicable in control of the satellite formation.

Description

technical field [0001] The invention relates to the field of aerospace measurement and control, in particular to a guidance method for a three-axis air bearing platform for verifying satellite formation. Background technique [0002] The full physical simulation of the satellite control system is a unique simulation method in the process of developing satellite control. It uses a three-axis air-floating turntable as a motion simulator, also known as air-floating table simulation. The full physical simulation of the satellite control system uses a three-axis air-floor platform 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. Air-floor table simulation is an ideal method, which can simulate this space environment well and is easy to r...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05D1/02
Inventor 林晓辉杨明张锦绣叶东董晓光
Owner HARBIN INST OF TECH
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