Lunar Soft - Landing Trajectory of Mechanics Optimization Based on the Improved Ant Colony Algorithm

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Abstract:

Based on research carried out for the most fuel-lunar soft landing trajectory optimization problem. First, by improving the function approximation method, the lunar soft landing trajectory optimization problem into a parameter optimization problem, and the optimization variables and state variables have a clear physical meaning. Then use the decimal ant colony algorithm adds local search strategy to study the optimization problem. Finally, the optimization algorithm to optimize term direction angle simulation and error analysis.

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446-449

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December 2014

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© 2015 Trans Tech Publications Ltd. All Rights Reserved

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