Satellite attitude track control test system and method

A technology of orbit control and satellite attitude, which is applied in the field of satellite attitude orbit control test system, can solve the problems that cannot meet the requirements of simulator remote automatic control simulator fault autonomous identification processing and automatic statistical processing of component test data, so as to avoid work efficiency Low cost, saving manpower time, improving safety and reliability

Active Publication Date: 2015-01-07
AEROSPACE DONGFANGHONG SATELLITE
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Problems solved by technology

[0006] To sum up, the existing satellite attitude and orbit control test system relies on manual methods, which can no longer meet the requirements of remot

Method used

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  • Satellite attitude track control test system and method
  • Satellite attitude track control test system and method
  • Satellite attitude track control test system and method

Examples

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Example Embodiment

[0030] The present invention is a networked satellite attitude orbit control test system with simulator remote control function, including: simulator intelligent controller, simulator remote client, simulator head, database server, dynamic simulation computer, deployment Box, interface box, telemetry display computer. Among them, the simulator intelligent controller is connected to the simulator remote client through the LAN bus, and the database server, dynamics simulation computer, and telemetry display computer are also connected on the LAN bus. The external master control computer is connected with the telemetry display computer. The expansion box and interface box are connected with the dynamic simulation computer.

[0031] The simulator intelligent controller includes a zero slot controller, a simulator working state acquisition module, a simulator drive signal module, and a simulator drive power amplifier module. The communication between the internal modules of the simu...

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Abstract

The invention provides a satellite attitude track control test system and method. The satellite attitude track control test system comprises a simulator head, a simulator intelligent controller and a simulator remote client side, wherein the simulator head is used for outputting simulation signals in a test and simulating the operating environment of a satellite to be tested; the simulator intelligent controller is connected with the simulator head, controls the operation of the simulator head and collects the work state of the simulator head, and the simulator remote client side is connected with the simulator intelligent controller, controls the operation of the simulator intelligent controller remotely and displays the work state of the simulator head; the simulator remote client side is connected with the simulator intelligent controller through a bus. The satellite attitude track control test system and method can realize a simulator remote control function, carry out remote control and state display through the simulator remote client side, realize unattended operation of a test site, and improve work efficiency.

Description

technical field [0001] The invention relates to the field of aerospace testing equipment, in particular to a satellite attitude orbit control testing system and a system testing method. Background technique [0002] The satellite attitude and orbit control (attitude orbit control) test system is used for the ground test of the satellite attitude and orbit control subsystem. Some simulators (such as solar simulators) in the traditional satellite attitude and orbit control test system are not connected to the test network, requiring staff to manually operate the simulator at the test site, and remote automatic control cannot be implemented. [0003] Moreover, if some simulators fail to work, it may cause harm to the products on the star. For example, if the heating module of the earth simulator fails and the heating module continues to heat, if measures are not taken in time, it will cause damage to the infrared earth sensor on the star; If the rotation does not stop after r...

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Application Information

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IPC IPC(8): G05B23/02G05B17/02G06F17/30B64G7/00
CPCG05B23/0218G05B23/0243
Inventor 卢彦杰曾鸿姜鼎李响宋明轩
Owner AEROSPACE DONGFANGHONG SATELLITE
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