Convex Optimization of Launch Vehicle Ascent Trajectory with Heat-Flux and Splash-Down Constraints
Author:
Funder
Agenzia Spaziale Italiana
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.A35194
Reference45 articles.
1. Optimum Steering Program for the Entry of a Multistage Vehicle Into a Circular Orbit
2. Numerical Study of Optimal Trajectories with Singular Arcs for an Ariane 5 Launcher
3. Design and Evaluation of a Three-Dimensional Optimal Ascent Guidance Algorithm
4. Closed-Loop Endoatmospheric Ascent Guidance
5. Optimal Control of Endoatmospheric Launch Vehicle Systems: Geometric and Computational Issues
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