霍尼韦尔/DND直升机综合导航系统(HINS)测试方案

IEEE Symposium on Position Location and Navigation. A Decade of Excellence in the Navigation Sciences Pub Date : 1990-03-20 DOI:10.1109/PLANS.1990.66179

J. Zywiel, C. Webb, H. Russell

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引用次数: 1

摘要

直升机综合导航系统(HINS)的先进开发模型(ADM)为加拿大国防部建造，并在霍尼韦尔先进技术中心(ATC)进行测试。该系统融合了其组件传感器的互补优势，从而实现快速对准和最佳导航精度。故障检测隔离和重新配置功能监视传感器健康状况，识别故障组件，并自动重新配置系统以最佳地集成其余组件，从而在传感器故障时提供性能的优雅降低。讨论了测试程序方法和测试结果。测试使HINS团队对导航系统设计和在实时系统中实现传感器混合算法的软件有了高度的信心。

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Test program for Honeywell/DND helicopter integrated navigation system (HINS)

The advanced development model (ADM) for the helicopter integrated navigation system (HINS) is built for the Canadian Department of National Defence and tested at the Honeywell Advanced Technology Centre (ATC). The system blends the complementary strengths of its components sensors, resulting in fast alignment and optimum navigation accuracy. A failure detection isolation and reconfiguration functionality monitors sensor health, identifies failed components, and automatically reconfigures the system to optimally integrate the remaining components, thus providing a graceful degradation of performance in the event of a sensor failure. Both the test program approach and the test results are discussed. The testing has given the HINS team a high degree of confidence in the navigation system design and in the software that implements the sensor blending algorithms in the real-time system.<>

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IEEE Symposium on Position Location and Navigation. A Decade of Excellence in the Navigation Sciences

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