Optimal trajectories for Earth-to-Mars flight

DOI10.1023/A:1022661519758zbMath0899.90163OpenAlexW119249394MaRDI QIDQ1379928

J. Ning

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

zbMATH Keywords

celestial mechanicsastrodynamicsflight mechanicssequential gradient-restoration algorithmlow Earth orbitarrival windowdeparture windowfour-body modellow Mars orbitoptimal transfer of a spacecraft

Mathematics Subject Classification ID

Related Items (2)

Optimal low-thrust orbital maneuvers via indirect swarming method ⋮ Instationary Heat-Constrained Trajectory Optimization of a Hypersonic Space Vehicle by ODE–PDE-Constrained Optimal Control

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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