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 :
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