Worst-Case Analysis of the X-38 Crew Return Vehicle Flight Control System
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چکیده
منابع مشابه
Limited Adaptive Authority Flight Control for the Crew Launch Vehicle
The control system of the NASA Crew Launch Vehicle is designed to meet performance and robustness requirements during its ascent flight phase. However, the controller bandwidth and the attainable level of robust performance is limited by the degree of flexibility inherent in the long and slender design that has been adopted for this vehicle. Since there remains a substantial degree of uncertain...
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ژورنال
عنوان ژورنال: Journal of Guidance, Control, and Dynamics
سال: 2001
ISSN: 0731-5090,1533-3884
DOI: 10.2514/2.4708