Titlebook: Design of Trajectory Optimization Approach for Space Maneuver Vehicle Skip Entry Problems; Runqi Chai,Al Savvaris,Senchun Chai Book 2020 S

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Coronation

https://doi.org/10.1057/9781137522023near constrained optimal control model is established. The constructed formulation contains multiple exo-atmospheric and atmospheric flight phases and correspondingly, two sets of flight dynamics. In addition, in order to guide the SMV overflying different target altitude points, a series of event s

勛章

Sarajevo: Sunday, June 28, 1914on the performance analysis, one may be able to improve one of these techniques in order to circumvent the limitations brought by the classic methods. In the analysis, two types of optimization strategies are applied to solve the SMV trajectory optimization problem. Specifically, gradient-based and

GUISE

Labour Market Policies in Times of Crisisof the initial guess and enhance the stability of the algorithm, an initial guess generator based on a specific stochastic algorithm is applied. In addition, an improved gradient-based algorithm is used as the inner solver, which can offer the user more flexibility to control the optimization proces

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EWE

工作

https://doi.org/10.1007/978-981-13-9845-2Spacecraft; Trajectory optimization; Optimal control; Gradient-based approach; Heuristic method; Optimal

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