Sequential convex programming method using adaptive mesh refinement for entry trajectory planning problem

Author:

Zhou Xiang,He Rui-Zhi,Zhang Hong-Bo,Tang Guo-Jian,Bao Wei-Min

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference41 articles.

1. An on-line guidance algorithm for high L/D hypersonic reentry vehicles;Zang;Aerosp. Sci. Technol.,2019

2. Stochastic gradient particle swarm optimization-based entry trajectory rapid planning for hypersonic glide vehicles;Li;Aerosp. Sci. Technol.,2018

3. Introducing computational guidance and control;Lu;J. Guid. Control Dyn.,2017

4. Online trajectory optimization for power system fault of launch vehicles via convex programming;Li;Aerosp. Sci. Technol.,2020

5. Discretization performance and accuracy analysis for the powered descent guidance problem;Malyuta,2019

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