The simplified identification strategy for parameters of composite load model constituted by ZIP load model in parallel with asynchronous motor is researched.
研究了ZIP负荷模型与感应电动机相并联的综合负荷模型参数的简化辨识策略。
Furthermore, the design of flight control system is simplified by the scheme proposed without changing the structure and parameters of controller in big flight envelope.
直接针对飞机的非线性模型设计的自抗扰控制器在很大的包线范围内不需要改变控制器的结构和参数，简化了设计过程。
Simplified controls allow operators to change test parameters quickly with the push of a switch and turn of a knob.
简化的控制使操作者能够通过开关和旋钮快速改变测试参数。
应用推荐