New Adaptive Mesh Refinement Strategy for Entry Guidance via Sequential Convex Programming

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This study focuses on the entry guidance problem, which is a highly nonlinear and constrained optimal control problem. The entry guidance problem is formulated as a nonlinear trajectory optimization problem with six-degrees-of-freedom dynamics, path constraints, and boundary constraints. The formulated problem is discretized and solved using sequential convex programming (SCP) with successive linearization. However, during the discretization process, conventional collocation methods encounter a challenge with high-frequency jittering in the control and bank angle profiles near active path constraints. Because the considered problem especially involves tight path constraints, the solution jittering issue becomes severe. Therefore, this study proposes a novel mesh refinement strategy to address this problem. Unlike conventional mesh refinement strategies based on interpolation error, the proposed approach resolves the convergence and solution jittering issue of the SCP framework by linking the direct and indirect methods with the costate estimation under successive linearization. Along with the development, we introduce a novel costate estimation method and provide proof of its validity. We present numerical simulation results of the proposed method and conduct a comparison with conventional approaches. The results obtained demonstrate successful mitigation of the solution jittering issue and a significant improvement in solution accuracy regarding compliance with the necessary conditions of optimality.
Publisher
AMER INST AERONAUTICS ASTRONAUTICS
Issue Date
2024-04
Language
English
Article Type
Article
Citation

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, v.47, no.4, pp.711 - 727

ISSN
0731-5090
DOI
10.2514/1.G006918
URI
http://hdl.handle.net/10203/319145
Appears in Collection
RIMS Journal PapersAE-Journal Papers(저널논문)
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