Distribution-Agnostic Robust Trajectory Optimization via Chance-Constrained Reinforcement Learning
Summary
A new distribution-agnostic robust trajectory-optimization framework is presented, employing chance-constrained reinforcement learning to manage uncertainty from initial conditions and process noise, requiring only sampleability. The system first computes a deterministic nominal trajectory offline. Reinforcement learning then robustifies this baseline through a structured affine closed-loop correction law, incorporating a feedforward control adjustment and time-varying feedback gains. Probabilistic feasibility is empirically enforced using rollout-based upper-tail quantiles, while terminal dispersion is regulated via covariance-feasibility penalties. The framework was assessed on a three-dimensional multi-impulse Earth-Mars transfer and a stochastic atmospheric pinpoint rocket landing. Results indicate competitive upper-tail fuel cost, preserved probabilistic feasibility, and the robustification scaffold's portability across heterogeneous spacecraft trajectory planning problems without core stochastic-control redesign.
Key takeaway
For aerospace engineers designing robust trajectories for complex spacecraft missions, this framework offers a compelling solution. It effectively manages diverse uncertainties, from initial conditions to process noise, while maintaining probabilistic feasibility and competitive fuel costs. You should consider integrating this distribution-agnostic, chance-constrained reinforcement learning approach to enhance mission reliability and reduce the need for extensive redesign across different trajectory planning problems.
Key insights
A chance-constrained reinforcement learning framework robustifies spacecraft trajectory optimization against diverse uncertainties using an affine closed-loop correction.
Principles
- Uncertainty requires only sampleability.
- Robustify nominal trajectories with RL.
- Enforce feasibility via upper-tail quantiles.
Method
Compute a nominal trajectory offline. Apply reinforcement learning to derive an affine closed-loop correction law. Enforce probabilistic feasibility using rollout-based upper-tail quantiles and regulate terminal dispersion via covariance-feasibility penalties.
In practice
- Apply to multi-impulse Earth-Mars transfers.
- Adapt for atmospheric rocket landings.
- Re-use core structure for diverse spacecraft.
Topics
- Trajectory Optimization
- Reinforcement Learning
- Chance-Constrained Control
- Robust Control
- Spacecraft Guidance
- Stochastic Control
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Editorial summary, takeaway, and curation by AIssential. Original article published by Takara TLDR - Daily AI Papers.