Cross-platform extendible satellite dynamic simulation test system
A dynamic simulation and testing system technology, applied in general control systems, control/regulation systems, instruments, etc., can solve problems such as poor scalability of source code portability, easy to update and maintain, reduce complexity, and reduce costs Effect
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- Publication Date
- 2012-02-15
- Estimated Expiration
- Not applicable · inactive patent
Smart Images
Figure 1 Figure 2 Figure 3
Abstract
Description
technical field
[0001] The invention relates to a satellite dynamic simulation test system, in particular to a cross-platform scalable satellite dynamic simulation test system. Background technique
[0002] Aerospace engineering has the characteristics of hugeness, complexity and high comprehensiveness. Before the satellite goes into space, it needs to do full component testing and system simulation, so as to check the design scheme and existing problems of the system. With the deepening of space exploration, there are more and more types and styles of satellites, and there have been multi-satellite space missions, such as formation flight, rendezvous and docking, inter-satellite detection and tracking, and inter-satellite on-orbit module replacement and filling. The existing attitude control simulation test system for a single type of single satellite can no longer meet the demand.
[0003] The existing full-physical simulation and semi-physical simulation satellite attitu...
Examples
Embodiment Construction
[0032] Such as figure 1 As shown, the system mainly includes three parts: satellite system simulator 1, flight environment and motion simulator 2, and operation monitoring and management system simulator 3. Satellite system simulator 1 is further divided into satellite attitude control system simulator 11 and satellite Fundamental Subsystem Simulator 12. Wherein, the flight environment and motion simulator 2 is composed of an environment simulator 21 and an orbit and attitude dynamics solver 22, which is used to simulate the satellite flight environment and flight dynamics process; the satellite attitude control system simulator 11 is used to simulate the satellite's Attitude control loop, including controller simulator 111, sensor simulator 112, and actuator simulator 113; satellite basic subsystem simulator 12, including power supply subsystem simulator 121 and telemetry remote control subsystem simulator 122; operation monitoring and management System 3 simulates the funct...