AODV protocol wireless intelligent network-based satellite attitude control simulation system

A technology of satellite attitude control and intelligent network, applied in the direction of attitude control, general control system, control/regulation system, etc., can solve the problems of small number of nodes (generally less than tens, increase the difficulty of realizing wireless self-organizing network on the ground, etc., to achieve Shorten the R&D cycle, improve flexibility and operability, and increase the effect of flexibility and operability

Inactive Publication Date: 2016-01-20
NAT UNIV OF DEFENSE TECH
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AI Technical Summary

Problems solved by technology

General terrestrial wireless ad hoc network routing protocols usually have to deal with complex and changeable node topologies. The large number of nodes and frequent and uncertain topological changes between nodes greatly increase the difficulty of realizing terrestrial wireless ad hoc networks; and the satellite at

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  • AODV protocol wireless intelligent network-based satellite attitude control simulation system
  • AODV protocol wireless intelligent network-based satellite attitude control simulation system
  • AODV protocol wireless intelligent network-based satellite attitude control simulation system

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Embodiment Construction

[0033] see figure 1 , figure 1 It is a schematic structural diagram of the present invention, and the satellite attitude control simulation system based on the AODV protocol wireless intelligent network includes a physical simulation system and a mathematical simulation system, and the mathematical simulation system is a simulation computer, and the fiber optic gyroscope mathematical model is arranged on the simulation computer , Mathematical model of reaction flywheel.

[0034] The physical simulation system includes a single-axis air bearing platform, wireless intelligent network nodes 1, 2, 3, 4 and 5, on-board computer, fiber optic gyroscope, reaction flywheel, battery and power control box. The on-board computer is connected with two wireless intelligent network nodes. The on-board computer communicates wirelessly with the fiber optic gyroscope and the reaction flywheel through the wireless intelligent network node 4; the on-board computer communicates wirelessly with the ...

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Abstract

The invention relates to an AODV protocol wireless intelligent network-based satellite attitude control simulation system. The satellite attitude control simulation system includes a physical simulation system and a mathematical simulation system; the mathematical simulation system is provided with an optical fiber gyroscope mathematical mode and a reaction flywheel mathematical model; the physical simulation system performs physical simulation of satellite pitching channel attitude control; the mathematical simulation system performs mathematical simulation of satellite rolling and yaw channel satellite control; the physical simulation system includes a single-axis air bearing table, wireless intelligent network nodes, a spaceborne computer, an optical fiber gyroscope, a reaction flywheel and a power source; and the optical fiber gyroscope, the spaceborne computer, the reaction flywheel and a simulation computer are respectively with one or a plurality of wireless intelligent network nodes and can communicate with each other through the wireless intelligent network nodes. The AODV protocol wireless intelligent network-based satellite attitude control simulation system of the invention has the advantages of high simulation flexibility, low cost and high implementation performance, and can improve the flexibility and the feasibility of a small satellite attitude control simulation test.

Description

technical field [0001] The invention belongs to the technical field of spacecraft simulation testing, and in particular relates to a semi-physical simulation system for spacecraft attitude control of a wireless self-organizing network. Background technique [0002] The satellite attitude control system occupies a very important position in the design of the satellite control system, so the simulation of the attitude control system has very important practical significance for speeding up the research progress of the satellite control system, shortening the development cycle, and improving the reliability of the control system. The semi-physical simulation is based on the full mathematical simulation, by introducing the on-board computer and the sensors and actuators that need to be considered into the control loop, and the other parts still use mathematical simulation. [0003] The traditional simulation system design method is to connect the sensors, on-board computer and a...

Claims

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Application Information

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IPC IPC(8): G05B17/02G05D1/08
Inventor 高玉东曾国强连一君涂开武罗涛吴国福项军华褚金钱韩大鹏税海涛李志军袁福
Owner NAT UNIV OF DEFENSE TECH
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