Evolutionary principles applied to mission planning problems

DOI10.1007/s10569-006-9052-7zbMath1162.70021OpenAlexW2050158999MaRDI QIDQ861357

Bruce A. Conway, Christian M. Chilan, Bradley J. Wall

Publication date: 29 January 2007

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

Full work available at URL: https://doi.org/10.1007/s10569-006-9052-7

zbMATH Keywords

Genetic algorithmsEvolutionary methodsMission planningTrajectory optimization

Mathematics Subject Classification ID

Control of mechanical systems (70Q05) Celestial mechanics (70F15) Orbital mechanics (70M20) Optimality conditions for problems involving ordinary differential equations (49K15)

Related Items

Genetic algorithms applied to the solution of hybrid optimal control problems in astrodynamics ⋮ A multi-objective approach to the design of low thrust space trajectories using optimal control ⋮ Optimal low-thrust trajectories to asteroids through an algorithm based on differential dynamic programming ⋮ Cooperative evolutionary algorithm for space trajectory optimization ⋮ Optimal switching strategy for radially accelerated trajectories

Uses Software

• SNOPT
• Fortran-GA

Cites Work

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• Discrete approximations to optimal trajectories using direct transcription and nonlinear programming
• Direct optimization using collocation based on high-order Gauss-Lobatto quadrature rules