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- W2066152262 abstract "This paper describes the results of the preflight evaluation of the guidance and control systems of the High Speed Flight Demonstrator Phase II (HSFD-II). Since the vehicle does not have a nominal trajectory because of its launch method, it is not appropriate to evaluate this system by the root sum square method. The present evaluation followed two approaches, using one standard and one custom designed analysis. The former comprised a Monte-Carlo simulation, single error analysis, sensitivity analysis, and linear analysis. The latter used emergency separation, release oscillation, and GPS receiver error. Although in some cases the Monte-Carlo simulation in the standard analysis showed a failure to satisfy mission requirements, detailed analysis indicates that the system would guide the vehicle through a successful flight experiment. This evaluation establishes that the system satisfies all mission requirements. The actual flight experiment was carried out and the guidance and control systems worked quite well. Based on the results of the preflight evaluation and the results of the flight, this paper concludes that the guidance and control systems of the vehicle was properly designed." @default.
- W2066152262 created "2016-06-24" @default.
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- W2066152262 date "2005-05-16" @default.
- W2066152262 modified "2023-10-16" @default.
- W2066152262 title "Evaluation of Guidance and Control System of High Speed Flight Demonstrator Phase II" @default.
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- W2066152262 doi "https://doi.org/10.2514/6.2005-3274" @default.
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