A Novel Approach for Optimal Trajectory Design with Multiple Operation Modes of Propulsion System, Part 1

TL;DR

This paper introduces the Composite Smooth Control framework to optimize hybrid propulsion systems with multiple operation modes, simplifying complex boundary-value problems for spacecraft trajectory design.

Contribution

The paper presents a new CSC framework that transforms hybrid control problems into smooth, differentiable problems, enabling easier and accurate trajectory optimization.

Findings

Successfully applied to a multi-year, multi-revolution spacecraft trajectory

Enables treatment of hybrid problems as smooth boundary-value problems

Improves optimization efficiency and accuracy for hybrid propulsion systems

Abstract

Efficient performance of a number of engineering systems is achieved through different modes of operation - yielding systems described as "hybrid", containing both real-valued and discrete decision variables. Prominent examples of such systems, in space applications, could be spacecraft equipped with 1) a variable-$I_{\text{sp}}$, variable-thrust engine or 2) multiple engines each capable of switching on/off independently. To alleviate the challenges that arise when an indirect optimization method is used, a new framework --- Composite Smooth Control (CSC) --- is proposed that seeks smoothness over the entire spectrum of distinct control inputs. A salient aftermath of the application of the CSC framework is that the original multi-point boundary-value problem can be treated as a two-point boundary-value problem with smooth, differentiable control inputs; the latter is notably easier to solve, yet can be made to accurately approximate the former hybrid problem. The utility of the CSC framework is demonstrated through a multi-year, multi-revolution heliocentric fuel-optimal trajectory for a spacecraft equipped with a variable-$I_{\text{sp}}$, variable-thrust engine.