Abstract
The neighboring optimal control problem for a singularly perturbed nonlinear system with state and control inequality constraints is investigated. The problem is formulated in a more general and different form and the various characteristic features of the analysis are discussed. Next, the analysis is presented to generate a "sky print" for ascent maneuver of a hypersonic vehicle such as X-33 for damage and/or failure conditions.
Original language | English (US) |
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Article number | 876947 |
Pages (from-to) | 3870-3874 |
Number of pages | 5 |
Journal | Proceedings of the American Control Conference |
Volume | 6 |
DOIs | |
State | Published - Dec 1 2000 |