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首页> 外文会议>Saint Petersburg International Conference on Integrated Navigation Systems; 20050523-25; Saint Petersburg(RU) >HARDWARE IN-THE-LOOP SIMULATION OF CELESTIAL NAVIGATION SYSTEM
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HARDWARE IN-THE-LOOP SIMULATION OF CELESTIAL NAVIGATION SYSTEM

机译：导航系统的硬件在环仿真

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摘要

As a result of high spaceflight laboratory fees, it is impractical to take star-pictures real time in order to debug star sensor and test the algorithms of star map identification. In order to test the capability of identification algorithm, develop the star sensor quickly, as well as to reduce the cost and to improve the efficiency of developments, a new type of hybrid simulation system for celestial navigation is proposed in the paper. The configurations, functions and features of the system are introduced. The implementation methods and the specifications of the system are presented. It has the feature of flexibility and expansibility. By use of the proposed hybrid simulation system, some algorithms of star map identification and attitude determination can be effectively tested and validated in this platform, at the same time, using the system to make the hybrid real-time test, it is very significative for researching the dynamic capability of aircraft and system characteristic.
机译：由于航天实验室费用高昂，因此无法实时拍摄星型图像以调试星型传感器并测试星型图识别算法。为了测试识别算法的能力，快速开发恒星传感器，降低成本，提高开发效率，提出了一种新型的天体混合仿真系统。介绍了系统的配置，功能和特性。介绍了系统的实现方法和规范。它具有灵活性和可扩展性的特征。利用所提出的混合仿真系统，可以在该平台上有效地测试和验证星图识别和姿态确定的一些算法，同时，利用该系统进行混合实时测试，对研究飞机的动态能力和系统特性。

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