3D geosynchronous transfer of a satellite: Continuation on the thrust

DOI10.1023/B:JOTA.0000004870.74778.aezbMath1066.70016OpenAlexW2000147007MaRDI QIDQ597206

J. Gergaud, Joseph Noailles, Jean-Baptiste Caillau

Publication date: 6 August 2004

Published in: Journal of Optimization Theory and Applications (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1023/b:jota.0000004870.74778.ae

zbMATH Keywords

parametric optimal controlminimum-time transfershooting procedure

Mathematics Subject Classification ID

Applications of optimal control and differential games (49N90) Automated systems (robots, etc.) in control theory (93C85) Control of mechanical systems (70Q05) Orbital mechanics (70M20)

Related Items

Differential continuation for regular optimal control problems ⋮ Minimum fuel control of the planar circular restricted three-body problem ⋮ Optimal control and applications to aerospace: some results and challenges ⋮ Solution space exploration of low-thrust minimum-time trajectory optimization by combining two homotopies ⋮ Geometric optimal control and applications to aerospace ⋮ Riemannian metric of the averaged energy minimization problem in orbital transfer with low thrust ⋮ Second order optimality conditions in the smooth case and applications in optimal control ⋮ Remarks on Quadratic Hamiltonians in Spaceflight Mechanics ⋮ Existence domain for solutions of optimal control problems for bounded-thrust spacecrafts

Uses Software

• ADIFOR
• SOCS
• BNDSCO

Cites Work

• Unnamed Item
• Unnamed Item
• Unnamed Item
• Abort landing in the presence of windshear as a minimax optimal control problem. II: Multiple shooting and homotopy
• Existence and multiple solutions of the minimum-fuel orbit transfer problem
• Numerical computation of optimal trajectories for coplanar, aeroassisted orbital transfer
• Sensitivity analysis for parametric control problems with control-state constraints
• Sensitivity analysis for time optimal orbit transfer
• Sufficient Optimality Conditions for Optimal Control Subject to State Constraints
• Coplanar control of a satellite around the Earth
• Second Order Sufficient Conditions for Optimal Control Problems with Free Final Time: The Riccati Approach