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      KCI등재 SCIE SCOPUS

      Integrated Guidance and Control for the Fixed-trim Vehicle against the Maneuvering Target

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      https://www.riss.kr/link?id=A106848137

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      다국어 초록 (Multilingual Abstract)

      From the view of the fixed-trim reentry vehicle (FTRV) application, the integrated guidance and control (IGC) design is a key challenge. In order to improve the performance of the FTRV against the maneuvering target, an IGC system combining with the v...

      From the view of the fixed-trim reentry vehicle (FTRV) application, the integrated guidance and control (IGC) design is a key challenge. In order to improve the performance of the FTRV against the maneuvering target, an IGC system combining with the virtual target and the filter is proposed in this paper. To investigate the dynamics of the FTRV against the maneuvering target, a 7-DOF mathematical model is established and the error angle is employed to describe the relative motion between the FTRV and the target. Considering the controllability of theFTRV, a nonlinear differentiable error angle command is presented and its influence on the terminal velocity is discussed. To deal with the contradiction between the limited maneuverability and the demand of high guidance accuracy, the actual target is taken place with the virtual target, of which acceleration is estimated by the ESO. For improving the performance of the virtual target position prediction, a rolling updating strategy is proposed and derived analytically. Then, the back-stepping based IGC system is designed with the virtual target and the filter. The finite-time convergence of the IGC system is proved via the Lyapunov stability theorem. The numerical simulation results show the effectiveness of the proposed IGC system for the FTRV against the maneuvering target with time-varying acceleration.

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      참고문헌 (Reference)

      1 L. L. Wang, "Spiral maneuver penetration trajectory for moving-mass reentry warhead" 37 (37): 1484-1493, 2016

      2 Q. Zhang, "Robust virtual target guidance for the fixed-trim vehicle under multiconstraints" 75 : 271-283, 2018

      3 L. Shi, "Prescribed performance slide mode guidance law with terminal line-of-sight angle constraint against maneuvering targets" 83 (83): 2101-2110, 2017

      4 S. Vaddi, "Numerical state-dependent Riccati equation approach for missile integrated guidance control" 39 (39): 699-703, 2009

      5 S. H. Seyedipour, "Nonlinear integrated guidance and control based on adaptive back-stepping scheme" 89 (89): 415-524, 2017

      6 D. Chwa, "Nonlinear disturbance observer based adaptive guidance law against uncertainties in missile dynamics and target maneuver" 54 (54): 1739-1749, 2018

      7 Y. N. Yang, "Neural network approximationbased nonsingular terminal sliding mode control for trajectory tracking of robotic airships" 54 : 192-197, 2016

      8 T. Petsopoulos, "Moving-mass roll control system for fixed-trim re-entry vehicle" 33 (33): 54-60, 1996

      9 R. D. Robinett III, "Moving mass trim control for aerospace vehicles" 19 (19): 1064-1070, 1996

      10 M. Z. Hou, "Integrated guidance and control of homing missile against ground fixed target" 21 (21): 162-168, 2008

      1 L. L. Wang, "Spiral maneuver penetration trajectory for moving-mass reentry warhead" 37 (37): 1484-1493, 2016

      2 Q. Zhang, "Robust virtual target guidance for the fixed-trim vehicle under multiconstraints" 75 : 271-283, 2018

      3 L. Shi, "Prescribed performance slide mode guidance law with terminal line-of-sight angle constraint against maneuvering targets" 83 (83): 2101-2110, 2017

      4 S. Vaddi, "Numerical state-dependent Riccati equation approach for missile integrated guidance control" 39 (39): 699-703, 2009

      5 S. H. Seyedipour, "Nonlinear integrated guidance and control based on adaptive back-stepping scheme" 89 (89): 415-524, 2017

      6 D. Chwa, "Nonlinear disturbance observer based adaptive guidance law against uncertainties in missile dynamics and target maneuver" 54 (54): 1739-1749, 2018

      7 Y. N. Yang, "Neural network approximationbased nonsingular terminal sliding mode control for trajectory tracking of robotic airships" 54 : 192-197, 2016

      8 T. Petsopoulos, "Moving-mass roll control system for fixed-trim re-entry vehicle" 33 (33): 54-60, 1996

      9 R. D. Robinett III, "Moving mass trim control for aerospace vehicles" 19 (19): 1064-1070, 1996

      10 M. Z. Hou, "Integrated guidance and control of homing missile against ground fixed target" 21 (21): 162-168, 2008

      11 Y. Chen, "Integrated guidance and control for microsatellite real-time automated proximity operations" 148 : 175-185, 2018

      12 N. F. Palumbo, "Integrated guidance and control for homing missiles" 25 (25): 121-139, 2004

      13 G. Hardy, "Inequalities" Cambridge University Press 1952

      14 L. L. Wang, "Guidance law with deceleration control for moving-mass reentry warhead" 230 (230): 2639-2653, 2016

      15 Ji-Peng Dong, "Guidance Laws against Towed Decoy Based on Adaptive Back-stepping Sliding Mode and Anti-saturation Methods" 제어·로봇·시스템학회 16 (16): 1724-1735, 2018

      16 K. D. Geng, "Design of rollingguidance law using virtual target with control of terminal azimuth for a fixed-trim vehicle" 38 (38): 320-325, 2015

      17 S. P. Bhat, "Continuous Finite-time stabilization of the translational and rotational double integrators" 43 (43): 1998

      18 Y. N. Yang, "Attitude regulation for unmanned quadrotors using adaptive fuzzy gain-scheduling sliding mode control" 54 : 208-217, 2016

      19 R. Mukherjee, "Attitude dynamics and control of moving mass multibody aeromanerver vehicle" 18-21, 2008

      20 Amit Kumar, "Anticipated Trajectory based Proportional Navigation Guidance Scheme for Intercepting High Maneuvering Targets" 제어·로봇·시스템학회 15 (15): 1351-1361, 2017

      21 Y. Zhang, "Adaptive terminal angle constraint interception against maneuvering targets with fast fixed-time convergence" 28 (28): 2996-3014, 2018

      22 H. Lu, "Adaptive back-stepping control for integrated guidance and control design with input constraints" 37-42, 2017

      23 Z. X. Li, "A vehicle rollingguidance law based on fixed trimmed angle of attack" 38 (38): 23-26, 2012

      24 Y. N. Yang, "A time-specified nonsingular terminal sliding mode control approach for trajectory tracking of robotic airships" 92 (92): 1359-1367, 2018

      25 M. Zhou, "A spiral-maneuver control method for a fixed-trim warhead" 38 (38): 1195-1203, 2017

      26 J. G. Guo, "A new sliding mode control for integrated missile guidance and control system" 78 : 54-61, 2018

      27 R. H. Byrnc, "A moving mass trim control system for reentry vehicle guidance" 644-650, 1996

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      학술지 이력

      학술지 이력
      연월일 이력구분 이력상세 등재구분
      2023 평가예정 해외DB학술지평가 신청대상 (해외등재 학술지 평가)
      2020-01-01 평가 등재학술지 유지 (해외등재 학술지 평가) KCI등재
      2010-01-01 평가 등재학술지 유지 (등재유지) KCI등재
      2009-12-29 학회명변경 한글명 : 제어ㆍ로봇ㆍ시스템학회 -> 제어·로봇·시스템학회 KCI등재
      2008-01-01 평가 등재학술지 유지 (등재유지) KCI등재
      2007-10-29 학회명변경 한글명 : 제어ㆍ자동화ㆍ시스템공학회 -> 제어ㆍ로봇ㆍ시스템학회
      영문명 : The Institute Of Control, Automation, And Systems Engineers, Korea -> Institute of Control, Robotics and Systems
      KCI등재
      2005-01-01 평가 등재학술지 선정 (등재후보2차) KCI등재
      2004-01-01 평가 등재후보 1차 PASS (등재후보1차) KCI등재후보
      2002-07-01 평가 등재후보학술지 선정 (신규평가) KCI등재후보
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      기준연도 WOS-KCI 통합IF(2년) KCIF(2년) KCIF(3년)
      2016 1.35 0.6 1.07
      KCIF(4년) KCIF(5년) 중심성지수(3년) 즉시성지수
      0.88 0.73 0.388 0.04
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