Implementation of Pitch Angle Controller For_2_4
Satellite Design Course Spacecraft Configuration Structural Design Preliminary Design Methods
Where: I T = moment of inertia of turbine rotor. T = angular shaft speed. T E = mechanical torque necessary to turn the generator. T A = aerodynamic.
Dr. Curran Crawford & Luke Stack Department of Mechanical Engineering University of Victoria 28 th ASME Wind Energy Symposium 47 th AIAA Aerospace Sciences.
1-s2.0-S1000936113000381-main
