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Volumn 1, Issue , 2006, Pages 369-391

Development of small unmanned aerial vehicle research platform: Modeling and simulating with flight test validation

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC MODELS; FLIGHT TESTS; SIMULATION MODELS; UNMANNED AERIAL VEHICLES;

EID: 33846535790     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (25)

References (20)
  • 3
    • 33746926416 scopus 로고    scopus 로고
    • MS Thesis, Department of Aeronautics and Astronautics, Massachusetts Institute of Technology, MA, September
    • King, E., Distributed Coordination and Control Experiments on a Multi-UAV Testbed, MS Thesis, Department of Aeronautics and Astronautics, Massachusetts Institute of Technology, MA, September 2004.
    • (2004) Distributed Coordination and Control Experiments on a Multi-UAV Testbed
    • King, E.1
  • 4
    • 74549201991 scopus 로고    scopus 로고
    • School of Aerospace Engineering, Georgia Institute of Technology, American Institute of Aeronautics and Astronautics, AIAA 2001-4059
    • Johnson, E., and Fontaine, S., "Use of Flight Simulation to Complement Flight Testing of Low-Cost UAVs," School of Aerospace Engineering, Georgia Institute of Technology, American Institute of Aeronautics and Astronautics, 2001, (AIAA 2001-4059).
    • (2001) Use of Flight Simulation to Complement Flight Testing of Low-Cost UAVs
    • Johnson, E.1    Fontaine, S.2
  • 5
    • 30744478253 scopus 로고    scopus 로고
    • rd AIAA Aerospace Sciences Meeting and Exhibit, January 2005, (AIAA 2005-1023).
    • rd AIAA Aerospace Sciences Meeting and Exhibit, January 2005, (AIAA 2005-1023).
  • 6
    • 33845247595 scopus 로고    scopus 로고
    • MS Thesis, AFIT/GAE/ENY/06-D05, School of Engineering and Management, Air Force Institute of Technology AU, Wright-Patterson AFB, OH, March
    • Higgs, Travis J. Modeling, Stability, and Control of a RotaTable Tail on a Micro Air Vehicle, MS Thesis, AFIT/GAE/ENY/06-D05, School of Engineering and Management, Air Force Institute of Technology (AU), Wright-Patterson AFB, OH, March 2006.
    • (2006) Modeling, Stability, and Control of a RotaTable Tail on a Micro Air Vehicle
    • Higgs, T.J.1
  • 8
    • 33846550769 scopus 로고    scopus 로고
    • Unmanned Aerial Vehicles Roadmap 2002-2027
    • Office of the Sectretary of Defense, December
    • Office of the Sectretary of Defense, Unmanned Aerial Vehicles Roadmap 2002-2027. Washington: HQ DOD, December. 2002.
    • (2002) Washington: HQ DOD
  • 9
    • 33846498644 scopus 로고    scopus 로고
    • SIG Manufacturing Company, Inc, Montezuma, IA
    • SIG Rascal 110 ARF Assembly Manual, SIG Manufacturing Company, Inc., Montezuma, IA.
    • SIG Rascal 110 ARF Assembly Manual
  • 10
    • 29744444481 scopus 로고
    • An Accurate Method of Measuring the Moments of Inertia of Airplanes
    • Washington DC, Langly Memorial Aeronautical Laboratory, October
    • Miller, M.P. An Accurate Method of Measuring the Moments of Inertia of Airplanes, Technical Notes: National Advisory Committee for Aeronautics, Washington DC, Langly Memorial Aeronautical Laboratory, #351, October, 1930.
    • (1930) Technical Notes: National Advisory Committee for Aeronautics , Issue.351
    • Miller, M.P.1
  • 14
    • 33846473244 scopus 로고    scopus 로고
    • Honeywell Technology Center, Application of Multivariable Control Theory to Aircraft Control Laws: Final Report, March 1993 - March 1996, Contract f33615-92-C-3607, Paper WL-TR-96-3099, Minneapolis, MN., May 1996 (ADAS 15259).
    • Honeywell Technology Center, "Application of Multivariable Control Theory to Aircraft Control Laws: Final Report, March 1993 - March 1996," Contract f33615-92-C-3607, Paper WL-TR-96-3099, Minneapolis, MN., May 1996 (ADAS 15259).
  • 17
    • 29244486527 scopus 로고    scopus 로고
    • Sadraey, M., and Colgren, R., UAV Flight Simulation: Credibility of Linear Decoupled vs. Nonlinear Coupled Equations of Motion, AIAA Modeling and Simulation Technologies Conference and Exhibit. August, 2005, (AIAA 2005-6425).
    • Sadraey, M., and Colgren, R., "UAV Flight Simulation: Credibility of Linear Decoupled vs. Nonlinear Coupled Equations of Motion," AIAA Modeling and Simulation Technologies Conference and Exhibit. August, 2005, (AIAA 2005-6425).
  • 18


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.