The LQ is adapted to the flight control law design such as the Normal Acceleration control system.
并以法向过载控制模态为例，将线性二次型运用到飞行控制系统的控制律设计中。
The correct control condition given in this paper is important to structure the practical field acceleration control system for induction motor.
本文得到的正确控制条件对于构成实际的控制系统具有重要意义。
Acceleration parameter is very important for train control system.
列车加速度对运行控制系统极为重要。
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