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- W2037231721 abstract "An optimal control problem is formulated for a maneuvering reentry vehicle to execute a maximum terminal velocity turn at constant altitude to a fixed final position. A control solution technique is devised which uses a Newton scheme to repetitively solve a nonlinear algebraic system for two parameters to provide the on-line guidance. The turn control takes advantage of the high dynamic pressure at the beginning of the flight path; the lift solution acts to null deviations from the prescribed altitude. Control solutions are compared for a continuously updated, approximate physical model, for a simulation of the approximate optimal guidance in a true physical model, and for a parameter optimization solution for the true model. End constraint satisfaction is excellent. Overall trajectory agreement is good, if the assumed atmospheric model is reasonably accurate." @default.
- W2037231721 created "2016-06-24" @default.
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- W2037231721 date "1987-08-17" @default.
- W2037231721 modified "2023-09-27" @default.
- W2037231721 title "Maximum terminal velocity turns at constant altitude" @default.
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- W2037231721 doi "https://doi.org/10.2514/6.1987-2566" @default.
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