CBC471 发表于 2025-3-25 04:07:23
http://reply.papertrans.cn/59/5865/586463/586463_21.png亚麻制品 发表于 2025-3-25 11:02:01
http://reply.papertrans.cn/59/5865/586463/586463_22.pngFemine 发表于 2025-3-25 14:17:24
Intelligent Systems, Control and Automation: Science and Engineeringhttp://image.papertrans.cn/l/image/586463.jpg爆米花 发表于 2025-3-25 19:42:09
http://reply.papertrans.cn/59/5865/586463/586463_24.png矿石 发表于 2025-3-25 21:41:10
http://reply.papertrans.cn/59/5865/586463/586463_25.png来就得意 发表于 2025-3-26 03:00:12
Simplified Rotor Dynamics,n characteristics and controls. Due to the complexity and the uncertainty associated with the aerodynamic phenomena, a detailed model of the forces and moments produced by the main rotor would be of high order and completely impractical for any controller design. In this Chapter, the modeling approaGRIEF 发表于 2025-3-26 05:31:27
Frequency Domain System Identification,his mathematical model is represented by a set of ordinary differential equations. Establishing such a model for helicopters is a challenging task. This Chapter provides a thorough description of a frequency domain identification procedure for the extraction of linear models that correspond to certa发酵 发表于 2025-3-26 11:47:47
http://reply.papertrans.cn/59/5865/586463/586463_28.png不舒服 发表于 2025-3-26 15:13:51
Time Domain Parameter Estimation and Applied Discrete Nonlinear Control for Small-Scale Unmanned Hel identification and control solution for direct application to an autonomous helicopter flight system. Although most controller designs are in continuous time, this Chapter considers the discrete time dynamics of the helicopter. The shift of the helicopter control problem to discrete time is twofol威胁你 发表于 2025-3-26 17:08:08
http://reply.papertrans.cn/59/5865/586463/586463_30.png