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.
- Publication:
-
Journal of Spacecraft and Rockets
- Pub Date:
- November 1977
- DOI:
- 10.2514/3.27991
- Bibcode:
- 1977JSpRo..14..676P
- Keywords:
-
- Algorithms;
- Newton-Raphson Method;
- Trajectory Analysis;
- Trajectory Optimization;
- Attitude Control;
- Decomposition;
- Mathematical Models;
- Orbits;
- Synchronous Satellites;
- Targets;
- Astrodynamics