Abstract
Low-thrust control technologies display advantages in space missions. In this study, a linearization method for constant-thrust control is proposed. Based on elliptic integrals, the constant-thrust linear equations are introduced. Furthermore, an analytical two-section linear equations are derived. In addition, for considering J 2 perturbation, semi-analytical linear equations are also presented. Numerical simulations are conducted to demonstrate the validation of the proposed method, which proves to be a practical choice for engineering.
| Original language | English |
|---|---|
| Article number | 012020 |
| Journal | Journal of Physics: Conference Series |
| Volume | 1786 |
| Issue number | 1 |
| DOIs | |
| State | Published - 24 Feb 2021 |
| Event | 2020 11th Asia Conference on Mechanical and Aerospace Engineering, ACMAE 2020 - Chengdu, Virtual, China Duration: 25 Dec 2020 → 27 Dec 2020 |
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