科研之友
微信
新浪微博
Facebook
分享链接
摘要
Elastic launch devices are widely used in aviation and aerospace, whereas the accurate assessment and practical control of their dynamic performance are often complicated. We propose and validate a metric approach to simplify the launch dynamics, regardless of unstable elastic parameters and various device distributions. The nonlinear relationship between main separation parameters and elastic potential energy is derived and quantified by the defined metric, which achieves the effective assessment and control of launch process in a simple way. The metric theory is proved by the actual ground tests of a typical launch using the pre-compressed spring devices. In addition, the approach has been successfully applied to evaluate and optimize TianTuo-1 satellite launch, reflecting small errors and easy operation in practical use.
- 出版日期2014-10
- 单位中国人民解放军国防科学技术大学
