In this paper, the optimization problem of reentry trajectory and aerodynamic heating history of the space shuttle has been discussed using the modern control theory by selecting the attack angle and the bank angle as control variables.
英
美
- 本文應用現代控制理論研究了航天飛行器三維最優(yōu)再入軌道和與軌道參數密切相關(guān)的氣動(dòng)加熱過(guò)程。
