The Adjoint Method and Its Application to Trajectory Optimization
Author:
Affiliation:
1. North American Aviation Inc., Downey, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Link
http://arc.aiaa.org/doi/pdf/10.2514/8.6284
Reference6 articles.
1. The Numerical Integration of Two-Point Boundary Value Problems
2. Gradient Theory of Optimal Flight Paths
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