This paper shall review the status, progress and results made in testing of the GN&C software and supporting avionics designed for the control of a large parafoil in support of the X-38 Program. This will include a high level overview of the GN&C design selected for use on the X-38 orbital return test article, as well as an overview of the requirements and test objectives for the parafoil flight portion of the orbital return flight, and of the testing results to date. These flight objectives will be mapped into flight and ground testing requirements and test beds currently in use by the X-38 Program, building sufficient confidence in the selected parafoil GN&C system, in order to proceed with the flight of the orbital test article. The X-38...
This paper gives an overview of the NASA F-18 High Alpha Research Vehicle. The three flight phases o...
The research and technology program of the civil air transportation system is reported. Research is ...
The slow flight speed, very light wing loading, and neutral stability of the Gossamer Condor and the...
NASA Dryden Flight Research Center and NASA Johnson Space Center are jointly conducting a phased pro...
During the final approach and landing phase of the X-38/Crew Return Vehicle, a steerable parafoil is...
First steps have been taken to qualify a family of parafoil systems capable of increasing the surviv...
Includes summary.Includes bibliographical references (leaves 70-73).Parafoils have been used in vari...
This thesis focuses on developing an autonomous parafoil steering system deployed from a near-space ...
During 2011 a series of progressively more challenging flight tests of the Mighty Eagle autonomous t...
The X-33 Guidance, Navigation, and Control (GN&C) Peer Review Team (PRT) was formed to assess the in...
Orbital testing requirements for guidance and control devices - technical descriptions for 30 possib...
The first test flight of the Orion Multi-Purpose Crew Vehicle presented additional challenges for gu...
The role parachutes have in many civil, humanitarian and military applications call for new and impr...
A free-flight investigation of a redio-controlled model of a manned reentry spacecraft with a telesc...
The first four flights of a remotely piloted airplane model showed that a flight envelope can be exp...
This paper gives an overview of the NASA F-18 High Alpha Research Vehicle. The three flight phases o...
The research and technology program of the civil air transportation system is reported. Research is ...
The slow flight speed, very light wing loading, and neutral stability of the Gossamer Condor and the...
NASA Dryden Flight Research Center and NASA Johnson Space Center are jointly conducting a phased pro...
During the final approach and landing phase of the X-38/Crew Return Vehicle, a steerable parafoil is...
First steps have been taken to qualify a family of parafoil systems capable of increasing the surviv...
Includes summary.Includes bibliographical references (leaves 70-73).Parafoils have been used in vari...
This thesis focuses on developing an autonomous parafoil steering system deployed from a near-space ...
During 2011 a series of progressively more challenging flight tests of the Mighty Eagle autonomous t...
The X-33 Guidance, Navigation, and Control (GN&C) Peer Review Team (PRT) was formed to assess the in...
Orbital testing requirements for guidance and control devices - technical descriptions for 30 possib...
The first test flight of the Orion Multi-Purpose Crew Vehicle presented additional challenges for gu...
The role parachutes have in many civil, humanitarian and military applications call for new and impr...
A free-flight investigation of a redio-controlled model of a manned reentry spacecraft with a telesc...
The first four flights of a remotely piloted airplane model showed that a flight envelope can be exp...
This paper gives an overview of the NASA F-18 High Alpha Research Vehicle. The three flight phases o...
The research and technology program of the civil air transportation system is reported. Research is ...
The slow flight speed, very light wing loading, and neutral stability of the Gossamer Condor and the...