Trajectory optimization and guidance for an advanced launch system
Author:
Affiliation:
1. Iowa State University of Science and Technology, Ames
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1992-732
Reference9 articles.
1. Finite Element Solution of Optimal Control Problems with Inequality Constraints
2. An Approach to Optimal Guidance of an Advanced Lauch Vehicle Concept
3. Robust Perturbation Guidance For The Advanced Launch System
4. Estimation of aerodynamics for slender bodies alone and with liftingsurfaces at alpha's from 0 deg to 90 deg.
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3. Near-Optimal Guidance and Pulse-Modulated Reduced-Attitude Control for Orbit Injection;Springer Optimization and Its Applications;2023
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