Comprehensive System Identification of Ducted Fan UAVs - Cal Poly
Comprehensive System Identification of Ducted Fan UAVs - Cal Poly
Comprehensive System Identification of Ducted Fan UAVs - Cal Poly
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Table 3.11 – MAV Wind Tunnel Identified Derivatives and Flight Test ResultsI-Star VehicleDerivative29”9”Wind TunnelFlight TestXu- 0.476 - 0.344 -0.1090Yv- 0.476(Fixed to X u )- 0.344(Fixed to X u )-0.1090(Fixed to X u )Zw- 0.349 - 0.212 n/aLv- 0.046(Fixed to –Mu)0.004(Fixed to –Mu)-0.5014(Fixed to –Mu)Lp0 0 0Mu0.046 0.003 0.5014Mq0 0 0Mpn/a n/a 0Lqn/a n/a 0Nw- 0.056 - 0.006 n/aNr0 n/a n/aXlon- 0.190 - 0.157 -0.2841Ylat0.156 0.123 n/aZcol- 0.012 - 0.264/100 n/aLlat- 0.218 - 0.418 n/aMlon- 0.387 - 0.548 -0.2343Nped0.669 0.555 n/aNcol-0.005 - 0.057/100 n/a- 44 -