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A Linear Domain System Identification for Small Unmanned Aerial Rotorcraft Based on Adaptive Genetic Algorithm 被引量:12

A Linear Domain System Identification for Small Unmanned Aerial Rotorcraft Based on Adaptive Genetic Algorithm
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摘要 This paper proposes a new adaptive linear domain system identification method for small unmanned aerial rotorcraft.Byusing the flash memory integrated into the micro guide navigation control module, system records the data sequences of flighttests as inputs (control signals for servos) and outputs (aircraft’s attitude and velocity information).After data preprocessing, thesystem constructs the horizontal and vertical dynamic model for the small unmanned aerial rotorcraft using adaptive geneticalgorithm.The identified model is verified by a series of simulations and tests.Comparison between flight data and the one-stepprediction data obtained from the identification model shows that the dynamic model has a good estimation for real unmannedaerial rotorcraft system.Based on the proposed dynamic model, the small unmanned aerial rotorcraft can perform hovering,turning, and straight flight tasks in real flight tests. This paper proposes a new adaptive linear domain system identification method for small unmanned aerial rotorcraft.Byusing the flash memory integrated into the micro guide navigation control module, system records the data sequences of flighttests as inputs (control signals for servos) and outputs (aircraft’s attitude and velocity information).After data preprocessing, thesystem constructs the horizontal and vertical dynamic model for the small unmanned aerial rotorcraft using adaptive geneticalgorithm.The identified model is verified by a series of simulations and tests.Comparison between flight data and the one-stepprediction data obtained from the identification model shows that the dynamic model has a good estimation for real unmannedaerial rotorcraft system.Based on the proposed dynamic model, the small unmanned aerial rotorcraft can perform hovering,turning, and straight flight tasks in real flight tests.
出处 《Journal of Bionic Engineering》 SCIE EI CSCD 2010年第2期142-149,共8页 仿生工程学报(英文版)
基金 supported by the State Key Program of National Natural Science of China(Grant No.60736025) the National Natural Science Foundation of China(Grant No.60905056) the National Basic Research Program of China(973 Program)(Grant No.2009CB72400102)
关键词 SMALL unmanned AERIAL ROTORCRAFT dynamic space MODEL MODEL identification adaptive GENETIC algorithm small unmanned aerial rotorcraft dynamic space model model identification adaptive genetic algorithm
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  • 1Wu H Y,Sun D,Zhou Z Y.Model identification of a micro air vehicle in loitering flight based on attitude performance evaluation[].IEEE Transactions on Robotics.2004
  • 2Hu C H,Huang X L,Hu J C,Zhu J H.System identification of a small UAV’s speeding up process before take-off[].th Asian Control Conference.2004
  • 3Mana1 M,Desbiens A,Gagnon E.Identification of a UAV and design of a hardware-in-the-loop system for nonlinear control purposes[].AIAA Guidance Navigation and Control Conference and Exhibit Unmanned Systems: Flight Control III.2005
  • 4Tischler M B.System identification methods for aircraft flight control development and validation[].Advances in Aircraft Flight Control.1996
  • 5Mettler B,Tischler M B,Kanade T.System identification of small-size unmanned helicopter dynamics[].American Heli- copter Society th Forum.1999
  • 6Salman S A,Sreenatha A G.Nonlinear identification of unmanned aircraft vehicle[].International Conference onAutomatic Control and System Engineering.2005
  • 7Klein V,Morelli E A.Aircraft System Identification: Theory and Practice[].AIAA.2006
  • 8Nelson R C.Flight Stability and Automatic Control[]..1989
  • 9Tischler M B,Remple R K.Aircraft and Rotorcraft System Identification: Engineering Methods with Flight-Test Ex- amples[].AIAA.2006
  • 10Marmion M.Airborne Attitude Estimation Using a Kalman Filter[]..2006

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