Add to ORKGThis thesis investigates the use of an integrator backstepping controller for a standard helicopter. First, a dynamic model of the helicopter in hovering condition is obtained through the use of Newton-Euler equations. Next, the idea of an integrator backstepping controller is examined followed by the derivation of the actual controller. Finally, simulation results from MATLAB are analyzed and potential future work is proposed
This work describes a model developed to analyze the aerodynamic loads on a helicopter model on conv...
This paper presents the results of attitude, velocity, heave and yaw controller design for an autono...
This document contains the study and application of a methodology in order to develop a controller f...
ii This thesis investigates the use of an integrator backstepping controller for a standard helicopt...
This thesis investigates the use of an integrator backstepping controller for a standard helicopter....
The control of quadrotor helicopter in a hover condition has always been a great challenge for contr...
The control of quadrotor helicopter in a hover condition has always been a great challenge for contr...
This paper presents the modelling and control of a laboratory helicopter system with MatLab. In this...
The objective of this paper is to present general techniques for simulating helicopter flight trajec...
Author's accepted manuscript (postprint).© 2019 IEEE. Personal use of this material is permitted. Pe...
Due to their highly coupled and non-linear behavior, helicopters seem excellent subjects to apply no...
In this paper, the dynamic model of quadrotor helicopter has been mathematically formulated. Then, a...
In this bachelor thesis, a nonlinear mathematical model simulation and linear controller design for ...
This paper present the results of attitude, velocity, heave and yaw controller design for UTM autono...
backstepping controller (IBC) is designed for the quadrotor altitude and attitude stabilization in t...
This work describes a model developed to analyze the aerodynamic loads on a helicopter model on conv...
This paper presents the results of attitude, velocity, heave and yaw controller design for an autono...
This document contains the study and application of a methodology in order to develop a controller f...
ii This thesis investigates the use of an integrator backstepping controller for a standard helicopt...
This thesis investigates the use of an integrator backstepping controller for a standard helicopter....
The control of quadrotor helicopter in a hover condition has always been a great challenge for contr...
The control of quadrotor helicopter in a hover condition has always been a great challenge for contr...
This paper presents the modelling and control of a laboratory helicopter system with MatLab. In this...
The objective of this paper is to present general techniques for simulating helicopter flight trajec...
Author's accepted manuscript (postprint).© 2019 IEEE. Personal use of this material is permitted. Pe...
Due to their highly coupled and non-linear behavior, helicopters seem excellent subjects to apply no...
In this paper, the dynamic model of quadrotor helicopter has been mathematically formulated. Then, a...
In this bachelor thesis, a nonlinear mathematical model simulation and linear controller design for ...
This paper present the results of attitude, velocity, heave and yaw controller design for UTM autono...
backstepping controller (IBC) is designed for the quadrotor altitude and attitude stabilization in t...
This work describes a model developed to analyze the aerodynamic loads on a helicopter model on conv...
This paper presents the results of attitude, velocity, heave and yaw controller design for an autono...
This document contains the study and application of a methodology in order to develop a controller f...