DocumentCode
2550275
Title
Expanding AirSTAR capability in an existing avionics design
Author
Laughter, S.A.
fYear
2012
fDate
14-18 Oct. 2012
Firstpage
1
Lastpage
20
Abstract
AirSTARis a UAS designed for flight dynamics and control research; Allows control law injection in-line with internal research pilot commands; Project development in a series of phases; Developed project UAV/RC experience; Developed LaRC policies and procedures; Phase-III utilized a commercial-of-the-shelf (COTS) airframe; Phase-IV flew a 5.5% dynamically scaled generic transport model (GTM) aircraft.
Keywords
avionics; project management; vehicle dynamics; AirSTAR capability; AirSTARis; COTS airframe; GTM aircraft; LaRC policies; Phase-III; Phase-IV flew; UAS; avionics design; commercial-of-the-shelf; control law injection; control research; flight dynamics; generic transport model; internal research pilot commands; project UAV/RC experience; project development;
fLanguage
English
Publisher
ieee
Conference_Titel
Digital Avionics Systems Conference (DASC), 2012 IEEE/AIAA 31st
Conference_Location
Williamsburg, VA
ISSN
2155-7195
Print_ISBN
978-1-4673-1699-6
Type
conf
DOI
10.1109/DASC.2012.6383122
Filename
6383122
Link To Document