Optimal trajectories for Earth-to-Mars flight
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Publication:1379928
DOI10.1023/A:1022661519758zbMath0899.90163OpenAlexW119249394MaRDI QIDQ1379928
Publication date: 5 March 1998
Published in: Journal of Optimization Theory and Applications (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1023/a:1022661519758
celestial mechanicsastrodynamicsflight mechanicssequential gradient-restoration algorithmlow Earth orbitarrival windowdeparture windowfour-body modellow Mars orbitoptimal transfer of a spacecraft
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Cites Work
- Primal-dual properties of sequential gradient-restoration algorithms for optimal control problems. II: General problem
- Sequential conjugate gradient-restoration algorithm for optimal control problems. I: Theory
- Modifications and extensions of the sequential gradient-restoration algorithm for optimal control theory
- Sequential gradient-restoration algorithm for the minimization of constrained functions. Ordinary and conjugate gradient versions
- Sequential gradient-restoration algorithm for optimal control problems
- Summary and comparison of several gradient-restoration algorithms for optimal control problems
- Robust predictor-corrector guidance for aeroassisted orbital transfer
- Near-optimal highly robust guidance for aeroassisted orbital transfer
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