NASA NTRS · 19780027940
A two-level trajectory decomposition algorithm featuring optimal intermediate target selection
Abstract
A decomposition algorithm is presented which optimizes complex missions by partitioning the trajectory into natural segments such as ascent or entry. Each segment defines a full-rank targeting subproblem. These are solved sequentially using the Newton-Raphson algorithm. The master problem, representing the complete mission, is to determine subproblem targets and master-problem controls that optimize the mission objective subject to intersegment constraints. The gradient projection algorithm solves this problem using derivatives obtained analytically from finite-difference subproblem sensitivities. Thus, the mission is optimized by coordinating the solution of tractible subproblems. Computational results for a synchronous equatorial mission are included.
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Petersen, F. M., Cornick, D. E., Brauer, G. L., Rehder, J. R.. 1977-11-01. A two-level trajectory decomposition algorithm featuring optimal intermediate target selection. https://ntrs.nasa.gov/citations/19780027940
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