Aiming at the optimization problem of spacecraft transfer trajectory, based on differential evolution algorithm, a fast optimization method for transfer trajectory with modified differential algorithm is proposed. The method can quickly find the best transfer trajectory that satisfies the specified constraints through the intelligent optimization based on the population individuals. It avoids the problems of large calculation and low efficiency caused by traditional iteration methods. The actual application of the calculation of the transfer trajectory under certain initial conditions shows that the method can quickly determine the transfer orbit parameters.
Calculation of Spacecraft Transfer Trajectory Based on Modified Differential Evolution Algorithm
Smart Innovation, Systems and Technologies
Advances in Smart Vehicular Technology, Transportation, Communication and Applications ; Chapter : 21 ; 219-227
2021-11-30
9 pages
Article/Chapter (Book)
Electronic Resource
English
NTRS | 1980
|Indirect Spacecraft Trajectory Optimization Using Modified Equinoctial Elements
Online Contents | 2010
Spacecraft trajectory optimization
TIBKAT | 2010
|