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Development of an Autonomous Flight Control System for Small Size Unmanned Helicopter Based on Dynamical Model 被引量:2
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作者 王赓 Kondak Konstantin +3 位作者 Marek Musial 盛焕烨 吕恬生 Hommel Günter 《Journal of Shanghai Jiaotong university(Science)》 EI 2007年第6期744-752,共9页
It is devoted to the development of an autonomous flight control system for small size unmanned helicopter based on dynamical model. At first, the mathematical model of a small size helicopter is described. After that... It is devoted to the development of an autonomous flight control system for small size unmanned helicopter based on dynamical model. At first, the mathematical model of a small size helicopter is described. After that simple but effective MTCV control algorithm was proposed. The whole flight control algorithm is composed of two parts: orientation controller based on the model for rotation dynamics and a robust position controller for a double integrator. The MTCV block is also used to achieve translation velocity control. To demonstrate the performance of the presented algorithm, simulation results and results achieved in real flight experiments were presented. 展开更多
关键词 unmanned HELICOPTER DYNAMICAL model FLIGHT control unmanned AERIAL vehicle (UAV)
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