메뉴 건너뛰기




Volumn 19, Issue 4, 1999, Pages 22-33

A Multidisciplinary Flight Control Development Environment and Its Application to a Helicopter

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER AIDED SOFTWARE ENGINEERING; COMPUTER GRAPHICS; COMPUTER PROGRAMMING; COMPUTER SIMULATION; CONTROL SYSTEM ANALYSIS; HELICOPTERS; INTERACTIVE COMPUTER SYSTEMS;

EID: 0032641646     PISSN: 1066033X     EISSN: None     Source Type: Journal    
DOI: 10.1109/37.777786     Document Type: Article
Times cited : (65)

References (21)
  • 1
    • 0004065446 scopus 로고    scopus 로고
    • Advances in Aircraft Flight Control
    • (Editor), Bristol, PA.: Taylor and Francis Ltd
    • M.B. Tischler (Editor), Advances in Aircraft Flight Control, Bristol, PA.: Taylor and Francis Ltd., 1996.
    • (1996)
    • Tischler, M.B.1
  • 2
    • 85008021742 scopus 로고    scopus 로고
    • Handling Qualities Requirements for Military Rotorcraft
    • ADS-33D, St. Louis, MO
    • United States Army Aviation Systems Command, “Handling Qualities Requirements for Military Rotorcraft,” ADS-33D, St. Louis, MO, 1996
    • (1996) United States Army Aviation Systems Command
  • 3
    • 85008037427 scopus 로고
    • Flying Qualities of Piloted Vehicles
    • MIL-STD-1797
    • United States Department of Defense, “Flying Qualities of Piloted Vehicles,” MIL-STD-1797, 1987.
    • (1987) United States Department of Defense
  • 5
    • 0025482438 scopus 로고
    • System Identification Requirements for High-Bandwidth Rotorcraft Flight Control System Design
    • M.B. Tischler, “System Identification Requirements for High-Bandwidth Rotorcraft Flight Control System Design,” J. Guidance, Control, and Dynamics, vol. 13, no. 5, pp. 835-841, 1990.
    • (1990) J. Guidance, Control, and Dynamics , vol.13 , Issue.5 , pp. 835-841
    • Tischler, M.B.1
  • 6
    • 0028126377 scopus 로고
    • Rotor-State Feedback in the Design of Flight Control Laws for a Hovering Helicopter
    • M.D. Takahashi, “Rotor-State Feedback in the Design of Flight Control Laws for a Hovering Helicopter,” J. American Helicopter Society, vol. 39, no. 1, pp. 52-62, 1994.
    • (1994) J. American Helicopter Society , vol.39 , Issue.1 , pp. 52-62
    • Takahashi, M.D.1
  • 8
    • 84997766067 scopus 로고
    • Preliminary Design Features of the RASCAL-A NASA/Army Rotorcraft In-Flight Simulator
    • AIAA Paper 92-41 75, August
    • E. Aiken, R. Jacobsen, M. Eshow, W. Hindson, and D. Doane, “Preliminary Design Features of the RASCAL-A NASA/Army Rotorcraft In-Flight Simulator,” AIAA Paper 92-41 75, August 1992.
    • (1992)
    • Aiken, E.1    Jacobsen, R.2    Eshow, M.3    Hindson, W.4    Doane, D.5
  • 9
    • 0005546484 scopus 로고    scopus 로고
    • CONDUIT-A New Multidisciplinary Integration Environment for Flight Control Development
    • AIAA Paper 97-3773, August
    • M.B. Tischler, J.D. Colbourne, M.R. Morel, D.J. Biezad, W.S. Levine, and V. Moldoveanu, “CONDUIT-A New Multidisciplinary Integration Environment for Flight Control Development,” AIAA Paper 97-3773, August 1997.
    • (1997)
    • Tischler, M.B.1    Colbourne, J.D.2    Morel, M.R.3    Biezad, D.J.4    Levine, W.S.5    Moldoveanu, V.6
  • 11
    • 85008033978 scopus 로고
    • CONSOL-OPTCADTM User's Manual
    • Version 1.2-1.5, Released May 1992), University of Maryland, College Park, MD
    • CONSOL-OPTCADTM User's Manual (Version 1.2-1.5, Released May 1992), University of Maryland, College Park, MD, 1992.
    • (1992)
  • 12
    • 0011084674 scopus 로고
    • Proposed Incorporation of Mission-Oriented Flying Qualities into MIL-STD 1797A
    • WL-TR-94-3162, October
    • D.G. Mitchell, and R.H. Hoh, “Proposed Incorporation of Mission-Oriented Flying Qualities into MIL-STD 1797A,” WL-TR-94-3162, October 1994.
    • (1994)
    • Mitchell, D.G.1    Hoh, R.H.2
  • 13
    • 50049084064 scopus 로고    scopus 로고
    • Moving Base Simulation Evaluation of Translational Rate Command Systems for STOVL Aircraft in Hover
    • NASA TM-110399, June
    • J.A. Franklin and M.W. Stortz, “Moving Base Simulation Evaluation of Translational Rate Command Systems for STOVL Aircraft in Hover,” NASA TM-110399, June 1996.
    • (1996)
    • Franklin, J.A.1    Stortz, M.W.2
  • 14
    • 0027578884 scopus 로고
    • On Combining Feasibility, Descent, and Superlinear Convergence in Equality Constrained Optimization
    • E.R. Panier, and A.L. Tits, “On Combining Feasibility, Descent, and Superlinear Convergence in Equality Constrained Optimization,” Mathematical Programming, vol. 59, pp. 261-276, 1993.
    • (1993) Mathematical Programming , vol.59 , pp. 261-276
    • Panier, E.R.1    Tits, A.L.2
  • 15
    • 0003997741 scopus 로고    scopus 로고
    • User's Guide for CFSQP Version 2.4: A C Code for Solving (Large Scale) Constrained Nonlinear (Minimax) Optimization Problems, Generating Iterates Satisfying All Inequality Constraints
    • University of Maryland, College Park, MD
    • C. Lawrence, J.L. Zhou, and A.L. Tits, “User's Guide for CFSQP Version 2.4: A C Code for Solving (Large Scale) Constrained Nonlinear (Minimax) Optimization Problems, Generating Iterates Satisfying All Inequality Constraints,” University of Maryland, College Park, MD, 1996.
    • (1996)
    • Lawrence, C.1    Zhou, J.L.2    Tits, A.L.3
  • 18
    • 0026889693 scopus 로고
    • Frequency-Response Method for Rotorcraft System Identification: Flight Applications to BO-105 Coupled Rotor/Fuselage Dynamics
    • M.B. Tischler and M.G. Cauffman, “Frequency-Response Method for Rotorcraft System Identification: Flight Applications to BO-105 Coupled Rotor/Fuselage Dynamics,” J. American Helicopter Society, vol. 37, no. 3, pp. 3-17, 1992.
    • (1992) J. American Helicopter Society , vol.37 , Issue.3 , pp. 3-17
    • Tischler, M.B.1    Cauffman, M.G.2
  • 19
    • 0029224744 scopus 로고
    • Identification of UH-60 Stability Derivative Models in Hover from Flight Test Data
    • J.W. Fletcher, “Identification of UH-60 Stability Derivative Models in Hover from Flight Test Data,” J. American Helicopter Society, vol. 40, no. 1, pp. 32-46, 1995.
    • (1995) J. American Helicopter Society , vol.40 , Issue.1 , pp. 32-46
    • Fletcher, J.W.1
  • 21
    • 0032114718 scopus 로고    scopus 로고
    • Roboust Multivariable Control of Rotorcraft in Forward Flight Impact of Bandwidth on Fatigue Life
    • J. N. Rorak and A. Ray, “Roboust Multivariable Control of Rotorcraft in Forward Flight Impact of Bandwidth on Fatigue Life,” J. American Hellcoptet Societv, vol 43, no 3, pp 195-201, 1998.
    • (1998) J. American Hellcoptet Societv , vol.43 , Issue.3 , pp. 195-201
    • Rorak, J.N.1    Ray, A.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.