This paper details the progress to date, toward developing a small autonomous helicopter. We describe system architecture, avionics, visual state estimation, custom IMU design, aircraft modelling, as well as various linear and neuro/fuzzy control algorithms. Experimental results are presented for state estimation using fused stereo vision and IMU data, heading control, and attitude control. FAM attitude and velocity controllers have been shown to be effective in simulation
The article focuses on different aspects (both theoretical and practical) of the development of the ...
In this report we determine the dynamic model of a miniature helicopter in hovering flight. Identifi...
This paper presents the results of attitude, velocity, heave and yaw controller design for an autono...
This paper details the progress to date, toward developing a small autonomous helicopter. We describ...
The indoor test bed of the Autonomous Systems Laboratory has been used to create a control system fo...
Summarization: This paper introduces a custom experimental test bed for the evaluation of autonomous...
UnrestrictedResearch on unmanned aerial vehicles is motivated by applications where human interventi...
The main characteristic attribute of the rotorcraft is the use of rotary wings to produce the thrust...
The main characteristic attribute of the rotorcraft is the use of rotary wings to produce the thrust...
Abstract: The paper addresses the design of an autopilot for small scale helicopters to let the vert...
We describe further progress towards the development of a MAV (micro aerial vehicle) designed as an ...
MIng (Computer and Electronic Engineering), North-West University, Potchefstroom Campus, 2014The use...
This paper details the design of an autonomous helicopter control system using a low cost sensor sui...
Abstract: This paper presents a new attitude stabilization and control of an unmanned helicopter ba...
Small Unmanned Aircraft Systems (UAS) are considered the stepping stone for the integration of civil...
The article focuses on different aspects (both theoretical and practical) of the development of the ...
In this report we determine the dynamic model of a miniature helicopter in hovering flight. Identifi...
This paper presents the results of attitude, velocity, heave and yaw controller design for an autono...
This paper details the progress to date, toward developing a small autonomous helicopter. We describ...
The indoor test bed of the Autonomous Systems Laboratory has been used to create a control system fo...
Summarization: This paper introduces a custom experimental test bed for the evaluation of autonomous...
UnrestrictedResearch on unmanned aerial vehicles is motivated by applications where human interventi...
The main characteristic attribute of the rotorcraft is the use of rotary wings to produce the thrust...
The main characteristic attribute of the rotorcraft is the use of rotary wings to produce the thrust...
Abstract: The paper addresses the design of an autopilot for small scale helicopters to let the vert...
We describe further progress towards the development of a MAV (micro aerial vehicle) designed as an ...
MIng (Computer and Electronic Engineering), North-West University, Potchefstroom Campus, 2014The use...
This paper details the design of an autonomous helicopter control system using a low cost sensor sui...
Abstract: This paper presents a new attitude stabilization and control of an unmanned helicopter ba...
Small Unmanned Aircraft Systems (UAS) are considered the stepping stone for the integration of civil...
The article focuses on different aspects (both theoretical and practical) of the development of the ...
In this report we determine the dynamic model of a miniature helicopter in hovering flight. Identifi...
This paper presents the results of attitude, velocity, heave and yaw controller design for an autono...