Complementarity-Gap-Driven Adaptive Sequential Convex Programming for Reentry Trajectory Optimization

To address the issue that existing penalty weight update strategies in the augmented Lagrangian multiplier method are disconnected from the optimality conditions and remain relatively sensitive to initial parameters, this paper proposes a complementarity-gap-driven adaptive sequential convex programming algorithm. The algorithm directly incorporates the complementarity slackness information from the KKT conditions into the parameter update laws. The defined complementarity slackness ratio and complementarity gap respectively measure the deviation of the current penalty intensity from the ideal multiplier level and the degree of departure from the complementarity slackness condition. Based on these two quantities, a bidirectional smooth update law for the penalty weight and a normalized gap update law for the multiplier are designed, which decouple the multiplier growth from the current multiplier magnitude. On this basis, a complete theoretical convergence framework is established, in which the monotonic bounded convergence of the Lagrange multiplier and the convergence of the slack variables and the complementarity gap are rigorously proved, and a conditional convergence theorem is given. Taking the reentry trajectory planning problem of a gliding vehicle as an example, numerical simulations are conducted with the initial penalty weight spanning five orders of magnitude. Simulation results demonstrate that the proposed algorithm converges rapidly and stably to the optimal solution satisfying the accuracy requirements under different initial weights, with the terminal position error stabilizing at 0.4–0.5 km, exhibiting favorable convergence accuracy. In addition, the stable convergence exhibited by the complementarity gap and the slackness radius validates the effectiveness and robustness of the complementarity-gap-driven adaptive update mechanism.

Authors

Institutions

Publication Details

Journal
Aerospace
Published
2026-09-14
DOI
https://doi.org/10.3390/aerospace13090838
Primary Topic
Spacecraft Dynamics and Control
Type
article
Field-Weighted Citation Impact
0.00
Controls
|||
ALL TIME
JAN
FEB
MAR
APR
MAY
JUN
JUL
AUG
SEP
article

Complementarity-Gap-Driven Adaptive Sequential Convex Programming for Reentry Trajectory Optimization

Guojian Tang, Leilei Wu, Chenglong Dong, Peng Wang
Aerospace
Spacecraft Dynamics and Control
article

Complementarity-Gap-Driven Adaptive Sequential Convex Programming for Reentry Trajectory Optimization

Guojian Tang, Leilei Wu, Chenglong Dong, Peng Wang
article en

Abstract

To address the issue that existing penalty weight update strategies in the augmented Lagrangian multiplier method are disconnected from the optimality conditions and remain relatively sensitive to initial parameters, this paper proposes a complementarity-gap-driven adaptive sequential convex programming algorithm. The algorithm directly incorporates the complementarity slackness information from the KKT conditions into the parameter update laws. The defined complementarity slackness ratio and complementarity gap respectively measure the deviation of the current penalty intensity from the ideal multiplier level and the degree of departure from the complementarity slackness condition. Based on these two quantities, a bidirectional smooth update law for the penalty weight and a normalized gap update law for the multiplier are designed, which decouple the multiplier growth from the current multiplier magnitude. On this basis, a complete theoretical convergence framework is established, in which the monotonic bounded convergence of the Lagrange multiplier and the convergence of the slack variables and the complementarity gap are rigorously proved, and a conditional convergence theorem is given. Taking the reentry trajectory planning problem of a gliding vehicle as an example, numerical simulations are conducted with the initial penalty weight spanning five orders of magnitude. Simulation results demonstrate that the proposed algorithm converges rapidly and stably to the optimal solution satisfying the accuracy requirements under different initial weights, with the terminal position error stabilizing at 0.4–0.5 km, exhibiting favorable convergence accuracy. In addition, the stable convergence exhibited by the complementarity gap and the slackness radius validates the effectiveness and robustness of the complementarity-gap-driven adaptive update mechanism.

AerospaceVol. 13(9)
New York State Department of Transportation (US), Hunan University (CN), National University of Defense Technology (CN)
Peace, Justice and strong institutions
Openalex Percentile: Top 7%
Spacecraft Dynamics and Control
AI Navigator

Ask Laika to Summarize, Analyze, and Connect papers live on the map.

Summarize Papers & Methodologies

Extract key findings, datasets, and comparative methods across publications.

Benchmark Rankings & Visual Analytics

Rank top research institutions, authors, funders, topics, and journals by Field-Weighted Citation Impact (FWCI) and paper volume with instant charts.

Connect Distant Disciplines

Bridge topological clusters on the map to find hidden collaborative intersections.