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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 1994, Vol. 15 ›› Issue (11): 1298-1305.

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A CALCULATION OF OPTIMAL FLIGHT TRAJECTORY USING THE PARAMETERIZED OPTIMIZATION METHOD

Liu Tongren   

  1. Faculty 509 of Beijing University of Aeronautics and Astronautics,Beijing 100083
  • Received:1992-02-25 Revised:1993-04-01 Online:1994-11-25 Published:1994-11-25

Abstract: An introduction is given to the transfonnation of optimal control problem with state inequality constraints,control inequality constraints and tenninal constraints into static nonlinear programming problem with parameterized optimization method, and a new augmented-SWIFT is also presented.The SWIFT(Sequential Weight-Increasing Factor Tech-nique)is used in static constrained optimization problem whereas the new auginented-SWIFT is extended to calculate dynamic constrained optimal control problem,Finally,the feasibility of this algorithm is certified by an example of a reentry optimal trajectory.

Key words: optimal control, parameterized optimization method, nonlinear programming, optimal flight trajectory

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