And the experimental tests had been carried out to verify the established model as well as the dynamic characteristics under opening loop control. 并通過(guò)實(shí)驗，對所建立的動(dòng)力學(xué)模型及開(kāi)環(huán)控制下平臺的實(shí)際動(dòng)態(tài)特性進(jìn)行了驗證。
For the finite propulsion reentry guidance, the conventional closed-thruster equation based on open-loop control loses its way. 摘要解決有限推力模型的再入飛行器初制導問(wèn)題，利用傳統開(kāi)環(huán)控制的關(guān)機方程達不到要求的精度。
