Autonomous precision placement of parafoils is challenging because of their limited control authority and sensitivity to winds. In particular, when wind speed is near the airspeed, guidance is further complicated by the parafoils inability to penetrate the wind. This article specifically addresses the terminal phase and develops an approach for generating optimal trajectories in real-time based on the inverse dynamics in the virtual domain. The method results in efficient solution of a two-point boundary-value problem using only a single optimization parameter allowing the trajectory to be generated at a high rate, mitigating effects of the unknown winds. It is shown through simulation and experimental results that the proposed algorithm wo...
The recent years have witnessed increased development of small, autonomous fixed-wing Unmanned Aeria...
Parafoil system is suitable for large-area and longtime surveillance and airdrop missions and has th...
Parafoil systems represent flexible wing vehicles. In case a vehicle is flying at low altitude, it i...
The article of record as published may be located at http://dx.doi.org/10.1243/09544100JAERO749Auton...
This paper deals with the development of guidance, navigation and control algorithms for a prototype...
Thesis (M.Sc.Eng.)Guided airdrop systems lacking propulsion may be adversely affected by high winds....
Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, vol. 225, no. 3, 2011...
Thesis: S.M., Massachusetts Institute of Technology, Department of Aeronautics and Astronautics, 201...
We present a framework for on-board trajectory planning and guidance for a large class of autonomous...
Winds can have a destabilizing effect on parafoil guidance and flight control. This paper will prese...
A guided ram-air parachute, or parafoil, offers a lightweight and efficient means for the autonomous...
This dissertation presents two contributions to the development of autonomous aerial delivery system...
Control of autonomous systems subject to stochastic uncertainty is a challenging task. In guided air...
An 8 degree-of-freedom model is developed that accurately models relative pitching and yawing motion...
Parafoil trajectory directly affects the power generation of a high-altitude wind power generation (...
The recent years have witnessed increased development of small, autonomous fixed-wing Unmanned Aeria...
Parafoil system is suitable for large-area and longtime surveillance and airdrop missions and has th...
Parafoil systems represent flexible wing vehicles. In case a vehicle is flying at low altitude, it i...
The article of record as published may be located at http://dx.doi.org/10.1243/09544100JAERO749Auton...
This paper deals with the development of guidance, navigation and control algorithms for a prototype...
Thesis (M.Sc.Eng.)Guided airdrop systems lacking propulsion may be adversely affected by high winds....
Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, vol. 225, no. 3, 2011...
Thesis: S.M., Massachusetts Institute of Technology, Department of Aeronautics and Astronautics, 201...
We present a framework for on-board trajectory planning and guidance for a large class of autonomous...
Winds can have a destabilizing effect on parafoil guidance and flight control. This paper will prese...
A guided ram-air parachute, or parafoil, offers a lightweight and efficient means for the autonomous...
This dissertation presents two contributions to the development of autonomous aerial delivery system...
Control of autonomous systems subject to stochastic uncertainty is a challenging task. In guided air...
An 8 degree-of-freedom model is developed that accurately models relative pitching and yawing motion...
Parafoil trajectory directly affects the power generation of a high-altitude wind power generation (...
The recent years have witnessed increased development of small, autonomous fixed-wing Unmanned Aeria...
Parafoil system is suitable for large-area and longtime surveillance and airdrop missions and has th...
Parafoil systems represent flexible wing vehicles. In case a vehicle is flying at low altitude, it i...