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Vehicle Health Management for Guidance, Navigation and Control Systems
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English
Abstract
The objective of the program was to architect a vehicle health management (VHM) system for space systems avionics that assures system readiness for launch vehicles and for space-based dormant vehicles. The platforms which were studied and considered for application of VHM for guidance, navigation and control (GN&C) included the Advanced Manned Launch System (AMLS), the Horizontal Landing-20/Personnel Launch System (HL-20/PLS), the Assured Crew Return Vehicle (ACRV) and the Extended Duration Orbiter (EDO). This set was selected because dormancy and/or availability requirements are driving the designs of these future systems.
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Authors
Citation
Radke, K., Frazzini, R., Bursch, P., Wald, J. et al., "Vehicle Health Management for Guidance, Navigation and Control Systems," SAE Technical Paper 932607, 1993, https://doi.org/10.4271/932607.Also In
References
- Coit David W. Priore Mary G. “Impact of Non-operating Periods on Equipment Reliability” ITT Research Institute RADC-TR-85-91 May 1985
- Johnson Stephen B. Puening Ron L. Obleski Maxine “System Health Management Design Methodology” Martin Marietta Space Launch Systems Company Purchase Order #F435025 14 July 1992
- “Reliability Prediction for Spacecraft,” RADC- TR-85-229 Rome Air Development Center 1985