Abstract
We present a procedure for the application of global orthogonal polynomial into an atmospheric re-entry maneuvering problem. This trajectory optimization is imbedded in a family of canonically parameterized optimal control problem. The optimal control problem is transcribed to nonlinear programming via global orthogonal polynomial and is solved a sparse nonlinear optimization algorithm. We analyze the optimal trajectories with respect to the performance of re-entry maneuver.
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Lee, D. Optimization analysis of trajectory for re-entry vehicle using global orthogonal polynomial. J Mech Sci Technol 20, 1557–1566 (2006). https://doi.org/10.1007/BF02916260
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DOI: https://doi.org/10.1007/BF02916260