Add to ORKGThis report describes a preliminary study on modeling and control of parafoil and payload systems with the twofold objective of developing tools for automatic testing and classification of parafoils and of devising autonomous paragliders able to accomplish long-range delivery or monitoring tasks. Three different models of decreasing complexity are derived and their accuracy compared by simulation
For parafoil and payload aircraft, control is affected by changing the length of several rigging lin...
The paper presents an initial move to develop a scalable high-degree-of-freedom model of the parafoi...
An investigation was made in the Langley Unitary Plan wind tunnel to determine the behavior of parag...
This report describes a preliminary study on modeling and control of parafoil and payload systems w...
For parafoil and payload aircraft, control is affected by changing the length of several rigging lin...
An 8 degree-of-freedom model is developed that accurately models relative pitching and yawing motion...
Guided parafoils arc composed of two primary bodies, a payload and parafoil. The payload encompasses...
Dynamic simulations are invaluable for studying system behavior, developing control models, and runn...
For parafoil and payload aircraft, control is affected by changing the length of several rigging lin...
A parafoil controlled by parafoil brake deflection offers a lightweight and space-efficient control ...
The design of remotely controlled and autonomous Un-manned Aerial Vehicles (UAVs) is an actual direc...
Controllable parafoil and payload aircraft are controlled with downward deflection of left and right...
This paper deals with the development of guidance, navigation and control algorithms for a prototype...
Abstract Numerous papers in the area of parafoil system design have been published over the past 50 ...
During the final approach and landing phase of the X-38/Crew Return Vehicle, a steerable parafoil is...
For parafoil and payload aircraft, control is affected by changing the length of several rigging lin...
The paper presents an initial move to develop a scalable high-degree-of-freedom model of the parafoi...
An investigation was made in the Langley Unitary Plan wind tunnel to determine the behavior of parag...
This report describes a preliminary study on modeling and control of parafoil and payload systems w...
For parafoil and payload aircraft, control is affected by changing the length of several rigging lin...
An 8 degree-of-freedom model is developed that accurately models relative pitching and yawing motion...
Guided parafoils arc composed of two primary bodies, a payload and parafoil. The payload encompasses...
Dynamic simulations are invaluable for studying system behavior, developing control models, and runn...
For parafoil and payload aircraft, control is affected by changing the length of several rigging lin...
A parafoil controlled by parafoil brake deflection offers a lightweight and space-efficient control ...
The design of remotely controlled and autonomous Un-manned Aerial Vehicles (UAVs) is an actual direc...
Controllable parafoil and payload aircraft are controlled with downward deflection of left and right...
This paper deals with the development of guidance, navigation and control algorithms for a prototype...
Abstract Numerous papers in the area of parafoil system design have been published over the past 50 ...
During the final approach and landing phase of the X-38/Crew Return Vehicle, a steerable parafoil is...
For parafoil and payload aircraft, control is affected by changing the length of several rigging lin...
The paper presents an initial move to develop a scalable high-degree-of-freedom model of the parafoi...
An investigation was made in the Langley Unitary Plan wind tunnel to determine the behavior of parag...