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Volumn 2005, Issue , 2005, Pages

A fault detection and reconfigurable control architecture for unmanned aerial vehicles

Author keywords

[No Author keywords available]

Indexed keywords

FEEDBACK LINEARIZATION; SWASH-PLATE ACTUATOR; UNMANNED AERIAL VEHICLES; UNMANNED ROTORCRAFT;

EID: 33751511730     PISSN: 1095323X     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1109/AERO.2005.1559597     Document Type: Conference Paper
Times cited : (51)

References (11)
  • 1
    • 0344894255 scopus 로고    scopus 로고
    • Tech. rep., Office of the Secretary of Defense, Washington, DC 20301
    • "Unmanned Aerial Vehicles Roadmap 2002-2027," Tech. rep., Office of the Secretary of Defense, Washington, DC 20301, 2002.
    • (2002) Unmanned Aerial Vehicles Roadmap 2002-2027
  • 5
    • 0042403667 scopus 로고    scopus 로고
    • Reconfigurable Helicopter Flight Control System
    • U. S. Patent 5,678,786, Oct.
    • Osder, S. S., "Reconfigurable Helicopter Flight Control System," U. S. Patent 5,678,786, Oct. 1997.
    • (1997)
    • Osder, S.S.1
  • 10
    • 0003476209 scopus 로고    scopus 로고
    • Ph.D. thesis, Georgia Institute of Technology, School of Aerospace Engineering, Atlanta, GA 30332, December
    • Johnson, E. N., Limited Authority Adaptive Flight Control, Ph.D. thesis, Georgia Institute of Technology, School of Aerospace Engineering, Atlanta, GA 30332, December 2000.
    • (2000) Limited Authority Adaptive Flight Control
    • Johnson, E.N.1
  • 11
    • 33644642299 scopus 로고    scopus 로고
    • Ph.D. thesis, Georgia Institute of Technology, School of Electrical and Computer Engineering, Atlanta, GA 30332, April
    • Clements, N. S., Fault Tolerant Control of Complex Dynamical Systems, Ph.D. thesis, Georgia Institute of Technology, School of Electrical and Computer Engineering, Atlanta, GA 30332, April 2003.
    • (2003) Fault Tolerant Control of Complex Dynamical Systems
    • Clements, N.S.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.