. This report describes the Caltech helicopter control experiment. The experiment consists of an electric model helicopter interfaced to and controlled by a PC. We describe the hardware and software. A state-space model for the angular position is identified from experimental data near hover, using the prediction error method. An LQR controller with integrators for set point tracking is designed for the system. We also undertake a separate identification and loop shaping control for the yaw dynamics. 1. Introduction This report describes the model helicopter experiment at the California Institute of Technology. The purpose of this report is to document our experience with the experiment, to facilitate the use in future projects. The Caltec...
At the Max Planck Institute for Biological Cybernetics the influence of an augmented system on helic...
Because of the largely nonlinear nature of the problem, controlling vehicles implies complicated con...
This paper presents the results of attitude, velocity, heave and yaw controller design for an autono...
This report describes the Caltech helicopter control experiment. The experiment consists of an elect...
This report describes the design and analysis of a control experiment to be implemented in the AERO ...
The goal of this paper is to describe a test bed for real-time helicopter flight control systems and...
MIng (Computer and Electronic Engineering), North-West University, Potchefstroom Campus, 2014The use...
The aim of this research project is to develop an autopilot system that enables the helicopter model...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76332/1/AIAA-1998-4357-315.pd
Making an RC helicopter perform hovering is one of the most challenging techniques that can be perfo...
In this thesis a dynamical model is developed for general six degrees of freedom quadrotor vehicle. ...
The scope of this report is the development of a mathematical model and a control system for a three...
In this paper we will introduce the existing model of a helicopter for teaching dynamic systems. Lat...
M.Ing.Linear control system theory is well developed and has lead to a number of control system type...
The Upturn was donated to Cal Poly in October 2012 by Neal Saiki from NTS. Our project was to replic...
At the Max Planck Institute for Biological Cybernetics the influence of an augmented system on helic...
Because of the largely nonlinear nature of the problem, controlling vehicles implies complicated con...
This paper presents the results of attitude, velocity, heave and yaw controller design for an autono...
This report describes the Caltech helicopter control experiment. The experiment consists of an elect...
This report describes the design and analysis of a control experiment to be implemented in the AERO ...
The goal of this paper is to describe a test bed for real-time helicopter flight control systems and...
MIng (Computer and Electronic Engineering), North-West University, Potchefstroom Campus, 2014The use...
The aim of this research project is to develop an autopilot system that enables the helicopter model...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76332/1/AIAA-1998-4357-315.pd
Making an RC helicopter perform hovering is one of the most challenging techniques that can be perfo...
In this thesis a dynamical model is developed for general six degrees of freedom quadrotor vehicle. ...
The scope of this report is the development of a mathematical model and a control system for a three...
In this paper we will introduce the existing model of a helicopter for teaching dynamic systems. Lat...
M.Ing.Linear control system theory is well developed and has lead to a number of control system type...
The Upturn was donated to Cal Poly in October 2012 by Neal Saiki from NTS. Our project was to replic...
At the Max Planck Institute for Biological Cybernetics the influence of an augmented system on helic...
Because of the largely nonlinear nature of the problem, controlling vehicles implies complicated con...
This paper presents the results of attitude, velocity, heave and yaw controller design for an autono...