Taylor polynomial-based constrained solver for fuel-optimal low-thrust trajectory optimisation
Thomas Caleb, Roberto Armellin, Spencer Boone, St\'ephanie Lizy-Destrez

TL;DR
This paper introduces a differential algebra-based framework for fuel-optimal low-thrust trajectory optimization, significantly reducing computation time while maintaining robustness and solution quality.
Contribution
It presents a novel DA-based approach combining DDP/iLQR and polynomial acceleration for efficient, robust constrained trajectory optimization in space missions.
Findings
Reduced run time by up to 88% in benchmarks
Systematic convergence of the most robust configuration
DA-based acceleration maintains solution quality and robustness
Abstract
This paper presents differential algebra-based differential dynamic programming (DADDy), a publicly available C++ framework for constrained, fuel-optimal low-thrust trajectory optimisation. The method uses differential algebra (DA) for two purposes: automatic differentiation and high-order Taylor expansions of the dynamics. These expansions replace many expensive numerical propagations with polynomial evaluations, reducing computational effort while preserving solution quality. The framework combines two complementary modules. First, a differential dynamic programming (DDP)/iterative linear-quadratic regulator (iLQR) stage computes an almost-feasible trajectory from imperfect initial guesses. Second, a polynomial-accelerated Newton stage enforces full feasibility with fast local convergence. Equality and inequality constraints are handled through an augmented Lagrangian formulation, and…
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