当前位置: X-MOL 学术J. Aerosp. Eng. › 论文详情
Our official English website, www.x-mol.net, welcomes your feedback! (Note: you will need to create a separate account there.)
Method for On-Orbit Thrust Estimation for Microthrusters Based on Nanosatellites
Journal of Aerospace Engineering ( IF 2.4 ) Pub Date : 2021-11-27 , DOI: 10.1061/(asce)as.1943-5525.0001370
Qinglin Yang 1 , Weijing Zhou 2 , Jifei Ye 3 , Hao Chang 4
Affiliation  

The development of nanosatellites is inseparable from micropropulsion systems, and a micropropulsion system cannot be separated from the evaluation of its micropropulsion performance. Although the ground measurement system is relatively mature, it ...

中文翻译:

基于纳米卫星的微型推进器在轨推力估计方法

纳米卫星的发展离不开微推进系统,而一个微推进系统也离不开对其微推进性能的评价。虽然地面测量系统相对成熟,但它...
更新日期:2021-11-27
down
wechat
bug