Hoekman, Bernard M. (Edt)/ Mav  | Michigan

0원  | 19970201  | 9780472108299

 | KS OmniScriptum Publishing

105,750원  | 20120809  | 9783659172229

Here a leading researcher provides a comprehensive treatment of the path following of Unmanned air vehicle(UAV) and coordinated target tracking. Firstly, it describes about the UAV, its definition, its uses, types of UAV and the system architecture of UAV. Different type of path following approaches discussed here. In vector field based trajectory tracking strategies have been discussed. An alternative to this is a nonlinear guidance system (PD controller approximation) as discussed.

 | Hutson Street Press

40,440원  | 20250522  | 9781025104164

In recent years, researchers have expressed a vested interest in the concepts surrounding flapping wing micro air vehicles(FWMAVs) that are capable of both range and complex maneuvering. Most research in this arena has found itself concentrated on topics such as flapping dynamics and the associated fluid-structure interactions inherent in the motion,however there still remains myriad questions concerning the structural qualities intrinsic to the wings themselves.

 | Hutson Street Press

59,830원  | 20250522  | 9781025099439

In recent years, researchers have expressed a vested interest in the concepts surrounding flapping wing micro air vehicles(FWMAVs) that are capable of both range and complex maneuvering. Most research in this arena has found itself concentrated on topics such as flapping dynamics and the associated fluid-structure interactions inherent in the motion,however there still remains myriad questions concerning the structural qualities intrinsic to the wings themselves.

Schafroth, Dario  | KS OmniScriptum Publishing

225,600원  | 20110726  | 9783838108698

Rotor and control design are two of the most challenging tasks during the development of an autonomous micro helicopter. Both areas are strongly affected by the extremely small size of the vehicle.The rotors are working in the low Reynolds numbers reducing efficiency and limiting the autonomy time of the helicopter. On the control side the small size leads to faster system dynamics and limits the payload for accurate sensors and actuators.

 | Springer

0원  | 19990501  | 9783540655718