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Volumn , Issue , 2007, Pages 1629-1633

Autopilot design of tilt-rotor UAV using particle swarm optimization method

Author keywords

Autopilot design; Particle swarm optimization; Tilt rotor UAV

Indexed keywords

CONTROL SYSTEM ANALYSIS; CONTROL THEORY; DESIGN; FLIGHT CONTROL SYSTEMS; LINEAR CONTROL SYSTEMS; MATHEMATICAL MODELS; OPTICAL COMMUNICATION; OPTIMIZATION; PARTICLE SWARM OPTIMIZATION (PSO); PNEUMATIC CONTROL EQUIPMENT; REQUIREMENTS ENGINEERING; SCHEDULING; SYSTEM STABILITY; THEOREM PROVING; UNMANNED AERIAL VEHICLES (UAV); VORTEX FLOW;

EID: 48349136106     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1109/ICCAS.2007.4406594     Document Type: Conference Paper
Times cited : (47)

References (13)
  • 1
    • 33646553368 scopus 로고    scopus 로고
    • Prop-rotor Load Evaluation in Collision Avoidance Maneuver of Tilt Rotor Unmanned Aerial Vehicle
    • Jan. 18-20
    • S. J. Hwang, M. K. Lee, Y. S. Kim & J. M. Kim, "Prop-rotor Load Evaluation in Collision Avoidance Maneuver of Tilt Rotor Unmanned Aerial Vehicle", AHS Vertical Lift Aircraft Design Conference, Jan. 18-20, 2006.
    • (2006) AHS Vertical Lift Aircraft Design Conference
    • Hwang, S.J.1    Lee, M.K.2    Kim, Y.S.3    Kim, J.M.4
  • 4
    • 0141946971 scopus 로고    scopus 로고
    • First Steps in the Development of Handling Qualities Criteria for a Civil Tiltrotor
    • Montreal, Canada, June 11-13
    • th Annual Forum, Montreal, Canada, June 11-13, 2002
    • (2002) th Annual Forum
    • Meyer, M.A.1    Padfield, G.D.2
  • 7
    • 0032071047 scopus 로고    scopus 로고
    • A Sliding Mode Missile Pitch Autopilot Synthesis for High Angle of Attack Maneuvering
    • Thukral, A. and Innocenti, M., "A Sliding Mode Missile Pitch Autopilot Synthesis for High Angle of Attack Maneuvering," IEEE Transaction on Control Systems Technique, Vol. 6, No. 3, 1998
    • (1998) IEEE Transaction on Control Systems Technique , vol.6 , Issue.3
    • Thukral, A.1    Innocenti, M.2
  • 8
    • 0347270158 scopus 로고    scopus 로고
    • A Robust Adaptive Nonlinear Control Approach to Missile Autopilot Design
    • Kim, S., Kim, Y., and Song, C., "A Robust Adaptive Nonlinear Control Approach to Missile Autopilot Design," Control Engineering Practice, Vol. 12, No. 2, 2004
    • (2004) Control Engineering Practice , vol.12 , Issue.2
    • Kim, S.1    Kim, Y.2    Song, C.3
  • 10
    • 48349104572 scopus 로고    scopus 로고
    • Rysdyk, R. T., Calise, A. J., and Chen, R. T. N., Nonlinear Adaptive Control of Tiltrotor Aircraft, AIAA/SAE World Aviation Congress 1997 Proceedings, Anaheim, CA, 1997
    • Rysdyk, R. T., Calise, A. J., and Chen, R. T. N., "Nonlinear Adaptive Control of Tiltrotor Aircraft," AIAA/SAE World Aviation Congress 1997 Proceedings, Anaheim, CA, 1997
  • 12
    • 1642303988 scopus 로고    scopus 로고
    • Reconfigurable Flight Control System Design Using Adaptive Neural Networks
    • Shin, D. H. and Kim, Y. D., "Reconfigurable Flight Control System Design Using Adaptive Neural Networks," IEEE Transactions on Control Systems Technology, Vol. 12, No. 1, 2004
    • (2004) IEEE Transactions on Control Systems Technology , vol.12 , Issue.1
    • Shin, D.H.1    Kim, Y.D.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.