Minimum-Time Earth-to-Mars Interplanetary Orbit Transfer Using Adaptive Gaussian Quadrature Collocation
Brittanny V. Holden, Shan He, Anil V. Rao

TL;DR
This paper presents a novel adaptive Gaussian quadrature collocation method for optimizing minimum-time low-thrust Earth-to-Mars transfers, demonstrating significant improvements over previous approaches in transfer duration.
Contribution
The study introduces a four-phase optimal control model and applies an adaptive collocation method, achieving faster transfer times than prior methods.
Findings
Minimum transfer times: 215, 196, and 198 days for the three models.
Transfer time improvements over previous work.
Detailed analysis of optimal solutions for different planetary motion models.
Abstract
The problem of minimum-time, low-thrust, Earth-to-Mars interplanetary orbital trajectory optimization is considered. The minimum-time orbital transfer problem is modeled as a four-phase optimal control problem where the four phases correspond to planetary alignment, Earth escape, heliocentric transfer, and Mars capture. The four-phase optimal control problem is then solved using a direct collocation adaptive Gaussian quadrature collocation method. The following three models are used in the study: (1) circular planetary motion; (2) elliptic planetary motion; and (3) elliptic planetary motion with gravity perturbations, where the transfer begins in a geostationary orbit and terminates in a Mars-stationary orbit. Results for all three cases are provided, and one particular case is studied in detail to show the key features of the optimal solutions. Using the particular value thrust…
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