Optimal ascent trajectories and feasibility of next-generation orbital spacecraft

DOI10.1023/A:1022633924359zbMath0945.70021MaRDI QIDQ1265016

K. Appert

Publication date: 3 October 2000

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

zbMATH Keywords

optimal trajectoriesflight mechanicsascent trajectoriesfeasibility regionfirst-stage structureimpulse/structural factor domainmaximum payload weight problemnonuniform structural factorrocket-powered spacecraftsecond-stage structuresingle-stage-to-orbit spacecraftspacecraft designtwo-stage-to-orbit spacecraftunfeasibility regionuniform structural factorzero-payload line

Mathematics Subject Classification ID

Variable mass, rockets (70P05) Orbital mechanics (70M20)

Related Items (6)

NEW APPROACH TO THE COLLISION AVOIDANCE PROBLEM FOR A SHIP ⋮ Multiple-subarc gradient-restoration algorithm. I: Algorithm structure ⋮ Multiple-subarc gradient-restoration algorithm. II: Application to a multistage launch vehicle design ⋮ Optimal control of a ship for course change and sidestep maneuvers ⋮ Optimal control of a ship for collision avoidance maneuvers ⋮ On feasibility of launch vehicle designs

Cites Work

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• Primal-dual properties of sequential gradient-restoration algorithms for optimal control problems. II: General problem
• Applied mathematics in aerospace science and engineering. Proceedings of the meeting held in Erice, Sicily, Italy, Sept. 3-10, 1991
• Primal and dual formulations of sequential gradient-restoration algorithms for trajectory optimization problems
• Optimization and acceleration guidance of flight trajectories in a windshear
• Gamma guidance schemes for flight in a windshear
• Robust predictor-corrector guidance for aeroassisted orbital transfer
• Near-optimal highly robust guidance for aeroassisted orbital transfer

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