Zobrazeno 1 - 6
of 6
pro vyhledávání: '"Sepehr Pourrezaei Khaligh"'
Autor:
Baris Fidan, A. H. Korayem, Anushya Viraliur Ponnuswami, Sepehr Pourrezaei Khaligh, Alireza Pazooki, Laleh Durali, Amir Khajepour
Publikováno v:
IEEE Transactions on Intelligent Transportation Systems. 23:7535-7546
In this paper, ultra-sonic sensors along with kinematics and dynamics equations of a towing vehicle are used to develop three approaches for hitch angle estimation. The first approach is based on direct calculation of hitch angle using certain a prio
Publikováno v:
Journal of the American Helicopter Society. 61:1-13
A fast inverse kinematic solution for the nonlinear actuating mechanisms of a small-scale helicopter
Publikováno v:
Multibody System Dynamics. 35:257-275
An inverse kinematic solution for the main rotor actuating mechanism of a small-scale helicopter that includes a four-point swashplate system and a Bell–Hiller mixer and the tail rotor actuating mechanism are derived using an approach that is suita
Publikováno v:
Journal of Intelligent & Robotic Systems. 73:289-308
A Hardware-In-The-Loop (HIL) testbed design for small unmanned helicopters which provides a safe and low-cost platform to implement control algorithms and tune the control gains in a controlled environment is described. Specifically, it allows for te
Publikováno v:
2013 International Conference on Unmanned Aircraft Systems (ICUAS).
A Hardware-In-The-Loop (HIL) testbed design for small unmanned helicopters is described. The testbed provides a safe and low-cost platform to implement control algorithms and tune the control gains in a controlled environment. Specifically, it allows
Publikováno v:
AIAA Modeling and Simulation Technologies Conference.
Helicopter aerodynamic modeling has always received growing attention especially in the applications such as model-based control design for the helicopter UAVs, in which the vehicle model is of utmost importance to obtain a satisfactory performance.