Abstract
The electric sail is a propellant-less propulsion system that utilizes the force exerted by the solar wind on the high-voltage tethers. This paper introduces a sequential convex programming (SCP) approach to solving the minimum-time continuous trajectory problem for the electric sail. The primary contribution is the transformation of the original non-convex optimal control problem into a convex program. Specifically, change of variables and a path constraint are introduced. Given that the final time is free, the path and terminal state constraints are convexified. The successive linearization technique transforms the nonlinear problem into a sequence of second-order cone programming problems, which are then solved iteratively by a successive solution algorithm. Numerical simulations of interplanetary transfers demonstrate the SCP approach's effectiveness and robustness, outperforming traditional direct methods.
| Original language | English |
|---|---|
| Pages (from-to) | 114-119 |
| Number of pages | 6 |
| Journal | IFAC-PapersOnLine |
| Volume | 59 |
| Issue number | 20 |
| DOIs | |
| State | Published - 1 Aug 2025 |
| Event | 23th IFAC Symposium on Automatic Control in Aerospace, ACA 2025 - Harbin, China Duration: 2 Aug 2025 → 6 Aug 2025 |
Keywords
- Electric solar wind sail
- Sequential Convex Programming
- Trajectory optimization
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