Trajectory Optimization and Guidance Methods for Mars Entry

Fundamental Knowledge.- Introduction.- Preliminaries.- Deterministic Optimization.- Improved Gauss pseudospectral method for Mars entry trajectory planning.- Improved sequential convex optimization for Mars entry trajectory planning.- Pseudospectral model predictive convex programming for Mars entry trajectory planning.- Indirect sequential convex programming for Mars entry trajectory planning.- Mars entry and powered descent using collaborative optimization.- Uncertainty optimization.- Mars entry trajectory optimization with desensitized optimal control.- Uncertainty quantification for Mars entry.- Robust trajectory optimization for Mars entry.- Robust optimal guidance method.- Direct model reference adaptive tracking guidance for Mars entry.- Computational guidance method for Mars entry.

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• Software matemático e estatístico
• Tecnologia aeronaval e aeroespacial
• Astronáutica
• Probabilidade e Estatística

Mars Entry, Descent, and Landing;Model Predictive Control;Trajectory Planning and Guidance;Robust Optimization;Computational Guidance;Uncertainty Qualification;Sequential Convex Programming;Pseudospectral Method;Predictor-Corrector Guidance;Desensitized Optimal Control