The invention belongs to the technical field of
rocket guidance, and provides a carrier
rocket trajectory optimization method based on an improved DE-SQP
algorithm to solve the technical problem that the expected purpose cannot be achieved when only a
heuristic algorithm is adopted to solve the problem of carrier
rocket ascending section
trajectory optimization under complex constraints at present. Comprising the following steps: S1, initializing parameters; s2, based on the step S1, performing
population initialization by adopting a Chebyshev
chaotic mapping fusion reverse learning strategy to obtain an initial
population; s3, performing updating iteration on the initial
population obtained in the step S2; s4, when an
algorithm termination criterion is met, stopping the updating
iteration process in the step S3, and outputting an individual with the highest fitness in the current population as an optimal solution; and S5, inputting the optimal solution obtained in the step S4 as an initial value into an SQP algorithm for solving, and outputting an
optimal trajectory. The method provided by the invention has strong
global optimization and local accurate search capabilities, and can effectively solve the problem of
trajectory optimization of the carrier rocket in the rising stage.