Online Reentry Trajectory Optimization Using Modified Sequential Convex Programming for Hypersonic Vehicle

Online Reentry Trajectory Optimization Using Modified Sequential Convex Programming for Hypersonic Vehicle

In this article, a highly nonlinear trajectory optimization problem for reentry vehicles is rapidly solved by the proposed modified sequential convex programming (MSCP) method. A logarithm linearization approach is proposed to decouple the dynamics of high order and nonconvex path constraints of hea...

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Bibliographic Details
Main Authors: Pei Pei, Shipeng Fan, Wei Wang, Defu Lin
Format: Article
Language:English
Published: IEEE 2021-01-01
Series:IEEE Access
Subjects:
Convex optimization
reentry trajectory
online optimization
aerodynamic uncertainties
no-fly zone constraint
Online Access:https://ieeexplore.ieee.org/document/9344608/

Internet

https://ieeexplore.ieee.org/document/9344608/

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