Successive Convexification of Non-Convex Optimal Control Problems and Its Convergence Properties
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Abstract (arXiv)
This paper presents an algorithm to solve non-convex optimal control problems, where non-convexity can arise from nonlinear dynamics, and non-convex state and control constraints. This paper assumes that the state and control constraints are already convex or convexified, the proposed algorithm convexifies the nonlinear dynamics, via a linearization, in a successive manner. Thus at each succession, a convex optimal control subproblem is solved. Since the dynamics are linearized and other constraints are convex, after a discretization, the subproblem can be expressed as a finite dimensional convex programming subproblem. Since convex optimization problems can be solved very efficiently, especially with custom solvers, this subproblem can be solved in time-critical applications, such as real-time path planning for autonomous vehicles. Several safe-guarding techniques are incorporated into the algorithm, namely virtual control and trust regions, which add another layer of algorithmic robustness. A convergence analysis is presented in continuous- time setting. By doing so, our convergence results will be independent from any numerical schemes used for discretization. Numerical simulations are performed for an illustrative trajectory optimization example.
Key facts. Cited by 10 papers in the map (data through 7 Oct 2026). First posted on arXiv 17 Aug 2016.
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Citing papers per year: 2023: 1; 2024: 1; 2025: 4; 2026: 4.
10 papers.
- 2023PRISE: Demystifying Deep Lucas-Kanade with Strongly Star-Convex Constraints for Multimodel Image Alignmentcited by 4
- 2025Agile Tradespace Exploration for Space Rendezvous Mission Design via Transformerscited by 4
- 2024Deep Loss Convexification for Learning Iterative Modelscited by 3
- 2025Deep Learning Warm Starts for Trajectory Optimization on the International Space Stationcited by 3
- 2025Language-Conditioned Safe Trajectory Generation for Spacecraft Rendezvouscited by 3
- 2026Intent-aligned Autonomous Spacecraft Guidance via Reasoning Modelscited by 1
- 2026Transformer-Based Warm-Starting for Feasible and Optimal Terminal Approach to Tumbling Objects with Space Manipulatorscited by 1
- 2025Tight Constraint Prediction of Six-Degree-of-Freedom Transformer-based Powered Descent Guidancecited by 0
- 2026Tempered Sequential Monte Carlo for Trajectory and Policy Optimization with Differentiable Dynamicscited by 0
- 2026Saturation-Aware Robust Trajectory Optimization for Reusable Launch Vehicles via Differentiable Physicscited by 0
- 2026Saturation-Aware Robust Trajectory Optimization for Reusable Launch Vehicles via Differentiable Physics2 Jul 2026
- 2026Transformer-Based Warm-Starting for Feasible and Optimal Terminal Approach to Tumbling Objects with Space Manipulators15 Jun 2026
- 2026Tempered Sequential Monte Carlo for Trajectory and Policy Optimization with Differentiable Dynamics23 Apr 2026
- 2026Intent-aligned Autonomous Spacecraft Guidance via Reasoning Models19 Apr 2026
- 2025Language-Conditioned Safe Trajectory Generation for Spacecraft Rendezvous9 Dec 2025
- 2025Agile Tradespace Exploration for Space Rendezvous Mission Design via Transformers3 Oct 2025
- 2025Deep Learning Warm Starts for Trajectory Optimization on the International Space Station8 May 2025
- 2025Tight Constraint Prediction of Six-Degree-of-Freedom Transformer-based Powered Descent Guidance1 Jan 2025
- 2024Deep Loss Convexification for Learning Iterative Models16 Nov 2024
- 2023PRISE: Demystifying Deep Lucas-Kanade with Strongly Star-Convex Constraints for Multimodel Image Alignment21 Mar 2023