학술논문

A Total Energy Control System strategy for the quadrotor helicopter
Document Type
Conference
Source
2015 International Conference on Unmanned Aircraft Systems (ICUAS) Unmanned Aircraft Systems (ICUAS), 2015 International Conference on. :286-293 Jun, 2015
Subject
Aerospace
Robotics and Control Systems
Vehicle dynamics
Aerodynamics
Helicopters
Vehicles
Mathematical model
Atmospheric modeling
Potential energy
Language
Abstract
This paper proposes a control strategy for the quadrotor helicopter based on the Total Energy Control System (TECS) approach. Assuming that the rotational dynamics control loop is faster than the translational dynamics control loop, a TECS based control strategy is designed for the translational dynamics. The performance of the proposed control strategy is verified experimentally.