First Principle Approach to Modeling of Primitive Quad Rotor
نویسندگان
چکیده
منابع مشابه
Dynamic Modeling and Control of Quad Rotor
Abstract This paper presents a nonlinear compensation technique to solve the trajectory tracking problem for a quadrotor. The kinematics and dynamic equations are obtained using Lagrange –Euler principle. The proposed control algorithm is robust to pay load variations even at high speed or low speeds. The controller can compensate the complex dynamics and also other external disturbances. The t...
متن کاملFirst Principle Approach to Modeling of Small Scale Helicopter
The establishment of global helicopter linear model is very precious and useful for the design of the linear control laws, since it is never afforded in the published literatures. In the first principle approach, the mathematical model was developed using basic helicopter theory accounting for particular characteristic of the miniature helicopter. No formal system identification procedures are ...
متن کاملReview: Modeling and Classical Controller Of Quad-rotor
This paper presents an overview of the most effective ideas for the Quad-rotor project. The concept of modeling using different methods is presented. The modeling part presented the nonlinear model, and the concept of linearization using small disturbance theory. Parameter identifications part explained the most important parameters that affect the system stability and tried to get suitable sol...
متن کاملModeling, Control and Navigation of an Autonomous Quad-rotor Helicopter
Autonomous outdoor quad-rotor helicopters increasingly attract the attention of potential researchers. Several structures and configurations have been developed to allow 3D movements. The quadrotor helicopter is made of a rigid cross frame equipped with four rotors. The autonomous quad-rotor architecture has been chosen for this research for its low dimension, good manoeuvrability, simple mecha...
متن کاملQuad-Rotor UAV: High-Fidelity Modeling and Nonlinear PID Control
Quad-rotor helicopter is an Unmanned Aerial Vehicle (UAV), whose lift is generated by four rotors located on the corner of X-shape. Due to simplicity of its dynamics and its ability to hover, quadrotor helicopter becomes as a popular platform for UAV. Current designs mostly consider a linear model for controller design. In this paper, we derivate nonlinear dynamic equations of the quadrotor UAV...
متن کاملذخیره در منابع من
با ذخیره ی این منبع در منابع من، دسترسی به آن را برای استفاده های بعدی آسان تر کنید
ژورنال
عنوان ژورنال: International Journal of Aeronautical and Space Sciences
سال: 2009
ISSN: 2093-274X
DOI: 10.5139/ijass.2009.10.2.148