Content
Frontiers of Information Technology & Electronic Engineering >> 2018, Volume 19, Issue 5 doi: 10.1631/FITEE.1700416
A composite optimization method for separation parameters of large-eccentricity pico-satellites
School of Aeronautics and Astronautics, Zhejiang University, Hangzhou 310027, China.
Abstract
Keywords
Pico-satellite ; Satellite–rocket separation mechanism ; Separation parameters ; Parameter optimization
Content