Abstract
This paper presents a multi-shooting analytical adaptive dynamic programming (MS-AADP) method for optimal trajectory design in the circular restricted three-body problem (CR3BP). This method integrates a multiple-shooting structure into the AADP framework, effectively combining the analytical tractability of AADP with improved convergence robustness enabled by multi-shooting. Besides, a novel bi-level framework is proposed that separates local control synthesis from global trajectory coordination, enabling efficient construction of segment-wise solutions and consistent optimization of inter-segment connections. In the inner level, a segment-wise analytical control law is derived based on a proposed Riccati-based AADP formulation, enabling efficient construction of local value functions. In the outer level, a stitched cost formulation is developed to optimize the intermediate shooting variables analytically, ensuring smooth inter-segment connections and global trajectory coherence. Numerical simulations of transfers between periodic orbits demonstrate the effectiveness and applicability of the proposed method in astrodynamics.
| Original language | English |
|---|---|
| Pages (from-to) | 2471-2476 |
| Number of pages | 6 |
| Journal | IFAC-PapersOnLine |
| Volume | 59 |
| Issue number | 20 |
| DOIs | |
| Publication status | Published - 1 Aug 2025 |
| Externally published | Yes |
| Event | 23th IFAC Symposium on Automatic Control in Aerospace, ACA 2025 - Harbin, China Duration: 2 Aug 2025 → 6 Aug 2025 |
Keywords
- Analytical Adaptive Dynamic Programming
- Bi-level Optimization
- Circular Restricted Three-Body Problem
- Low-thrust transfer
- Multiple shooting
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