Interplanetary gravity-assist fuel-optimal trajectory optimization with planetary and Solar radiation pressure perturbations

DOI10.1007/S10569-020-9955-8zbMath1448.70087OpenAlexW3009269233MaRDI QIDQ2004690

Mohammadreza Saghamanesh, Ehsan Taheri, He-Xi Baoyin

Publication date: 7 October 2020

Published in: Celestial Mechanics and Dynamical Astronomy (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s10569-020-9955-8

zbMATH Keywords

homotopy methodfull ephemeris modelfuel-optimalgravity-assisthigh-fidelity optimizationlow-thrust trajectory optimization

Mathematics Subject Classification ID

Numerical methods based on necessary conditions (49M05) Applications of optimal control and differential games (49N90) Variable mass, rockets (70P05) Optimality conditions for problems involving ordinary differential equations (49K15)

Cites Work

• A survey of methods available for the numerical optimization of continuous dynamic systems
• A multi-objective approach to the design of low thrust space trajectories using optimal control
• Cooperative evolutionary algorithm for space trajectory optimization
• New challenges to trajectory design by the use of electric propulsion and other new means of wandering in the solar system
• Studying the errors in the estimation of the variation of energy by the ``patched-conics model in the three-dimensional swing-by
• Survey of Numerical Methods for Trajectory Optimization
• Discrete approximations to optimal trajectories using direct transcription and nonlinear programming
• Adjoint variable solutions via an auxiliary optimization problem
• Finite difference scheme for automatic costate calculation
• New smoothing techniques for solving bang–bang optimal control problems—numerical results and statistical interpretation

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