Delta-V and ground metric investigations for responsive satellite formation flying
This paper studies a responsive mission involving a dual spacecraft flying formation system. A graphical solution based on the selective dependent variables for acquiring the local and global optimum impulsive velocities is proposed to obtain the minimum orbital transfer velocity changes as well as...
Saved in:
Main Authors: | Yahya, Nor Affendy, Varatharajoo, Renuganth, Harithuddin, A. S. M., Razoumny, Yury |
---|---|
Format: | Article |
Published: |
Elsevier
2022
|
Online Access: | http://psasir.upm.edu.my/id/eprint/100888/ https://www.sciencedirect.com/science/article/pii/S0094576521006688 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
Spacecraft formation flying responsive mission optimum Delta-V and ground performance measures
by: Yahya, Nor Affendy
Published: (2022) -
Performance measure of satellite flying in coplanar and non-coplanar formation
by: Yahya, Nor Affendy, et al.
Published: (2018) -
Disturbance observer-based fuzzy control for flexible spacecraft combined attitude & sun tracking system
by: Chak, Yew Chung, et al.
Published: (2017) -
Quasi-satellite system for leader-follower spacecraft formation
by: Mohd Harithuddin, Ahmad Salahuddin
Published: (2016) -
An optimum magnetic control torque generation of a momentum bias satellite
by: Suhadis, Nurulasikin, et al.
Published: (2014)