Fuel-optimal low-thrust CAM with eclipse constraints

被引：0

作者：

Polli, Eduardo Maria ^{[1
]}

Gonzalo, Juan Luis ^{[1
]}

Colombo, Camilla ^{[1
]}

机构：

[1] Politecn Milan, Via La Masa 34, I-20156 Milan, Italy

来源：

AEROSPACE SCIENCE AND ENGINEERING, IV AEROSPACE PHD-DAYS 2024 | 2024年 / 42卷

关键词：

Collision Avoidance Manoeuvre; Low Thrust; Optimal Control; Collision Probability; Space Traffic Management;

D O I：

10.21741/9781644903193-35

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

This works presents an optimal control direct method to design fuel-optimal low-thrust Collision Avoidance Manoeuvres (CAMs), imposing return to nominal conditions and including eclipse constraints. The methodology exploits the Hermite-Simpon integration scheme to impose the dynamics and the Squared Mahalanobis Distance (SMD) to ensure a collision probability lower than a prescribed value. The choice of using a direct method to solve the Optimal Control Problem (OCP) is justified by the inclusion of orbital perturbations.

引用

页码：158 / 161

页数：4

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