Output-feedback Synthesis Orbit Geometry: Quotient Manifolds and LQG Direct Policy Optimization
<|reference_start|>Output-feedback Synthesis Orbit Geometry: Quotient Manifolds and LQG Direct Policy Optimization: We consider direct policy optimization for the linear-quadratic Gaussian (LQG) setting. Over the past few years, it has been recognized that the landscape of dynamic output-feedback controllers of relevance to LQG has an intricate geometry, particularly pertaining to the existence of degenerate stationary points, that hinders gradient methods. In order to address these challenges, in this paper, we adopt a system-theoretic coordinate-invariant Riemannian metric for the space of dynamic output-feedback controllers and develop a Riemannian gradient descent for direct LQG policy optimization. We then proceed to prove that the orbit space of such controllers, modulo the coordinate transformation, admits a Riemannian quotient manifold structure. This geometric structure--that is of independent interest--provides an effective approach to derive direct policy optimization algorithms for LQG with a local linear rate convergence guarantee. Subsequently, we show that the proposed approach exhibits significantly faster and more robust numerical performance as compared with ordinary gradient descent.<|reference_end|>
@article{kraisler2024output-feedback,
    title={Output-feedback Synthesis Orbit Geometry: Quotient Manifolds and LQG
  Direct Policy Optimization},
    author={Spencer Kraisler and Mehran Mesbahi},
    journal={IEEE Control Systems Letters, vol. 8, pp. 1577-1582, 2024},
    year={2024},
    doi={10.1109/LCSYS.2024.3414962},
    archivePrefix={arXiv},
    eprint={2403.17157},
    primaryClass={math.OC cs.SY eess.SY}
}