Guided Policy Search using Sequential Convex Programming for Initialization of Trajectory Optimization Algorithms
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Abstract (arXiv)
Nonlinear trajectory optimization algorithms have been developed to handle optimal control problems with nonlinear dynamics and nonconvex constraints in trajectory planning. The performance and computational efficiency of many trajectory optimization methods are sensitive to the initial guess, i.e., the trajectory guess needed by the recursive trajectory optimization algorithm. Motivated by this observation, we tackle the initialization problem for trajectory optimization via policy optimization. To optimize a policy, we propose a guided policy search method that has two key components: i) Trajectory update; ii) Policy update. The trajectory update involves offline solutions of a large number of trajectory optimization problems from different initial states via Sequential Convex Programming (SCP). Here we take a single SCP step to generate the trajectory iterate for each problem. In conjunction with these iterates, we also generate additional trajectories around each iterate via a feedback control law. Then all these trajectories are used by a stochastic gradient descent algorithm to update the neural network policy, i.e., the policy update step. As a result, the trained policy makes it possible to generate trajectory candidates that are close to the optimality and feasibility and that provide excellent initial guesses for the trajectory optimization methods. We validate the proposed method via a real-world 6-degree-of-freedom powered descent guidance problem for a reusable rocket.
Key facts. Cited by 5 papers in the map (data through 14 Oct 2026). First posted on arXiv 13 Oct 2021.
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Citing papers per year: 2023: 1; 2024: 0; 2025: 0; 2026: 4.
5 papers.
- 2023Improving Computational Efficiency for Powered Descent Guidance via Transformer-based Tight Constraint Predictioncited by 5
- 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
- 2026OrbitTAMP: Grounding Language Models for Task and Motion Planning in Spacecraft Rendezvouscited by 0
- 2026Spacecraft Rendezvous Trajectory Generation with Modular Constraints via Diffusion Model Compositioncited by 0
- 2026Spacecraft Rendezvous Trajectory Generation with Modular Constraints via Diffusion Model Composition5 Oct 2026
- 2026OrbitTAMP: Grounding Language Models for Task and Motion Planning in Spacecraft Rendezvous1 Oct 2026
- 2026Transformer-Based Warm-Starting for Feasible and Optimal Terminal Approach to Tumbling Objects with Space Manipulators15 Jun 2026
- 2026Intent-aligned Autonomous Spacecraft Guidance via Reasoning Models19 Apr 2026
- 2023Improving Computational Efficiency for Powered Descent Guidance via Transformer-based Tight Constraint Prediction9 Nov 2023