지원사업
학술연구/단체지원/교육 등 연구자 활동을 지속하도록 DBpia가 지원하고 있어요.
커뮤니티
연구자들이 자신의 연구와 전문성을 널리 알리고, 새로운 협력의 기회를 만들 수 있는 네트워킹 공간이에요.
논문 기본 정보
- 자료유형
- 학술저널
- 저자정보
- 발행연도
- 2024.12
- 수록면
- 1,329 - 1,339 (11page)
- DOI
- 10.5302/J.ICROS.2024.24.0241
이용수
초록· 키워드
오류제보하기
This paper provides a longitudinal control loop design method for hypersonic vehicles based on feedback linearization control (FBLC) in combination with disturbance observer-based control (DOBC). Based on an analysis of the dynamics of hypersonic vehicles and their model uncertainties, a cascade control structure consisting of flight path angle, acceleration, and pitch rate control loops is herein proposed. A pitch rate control loop was designed to compensate for model uncertainties caused by aerodynamic model errors and unknown propulsion-aerodynamic coupling effects. These model uncertainties were estimated through the DOBC technique in the proposed method. Additionally, the behavior of the tracking errors and observer estimation errors in the control loop was analyzed using the Lyapunov stability theory. To provide useful insights into the proposed control loop, the connections between the proposed control loop structure and conventional control loop structures were examined. The proposed control loop was found to be equivalent to a 3-loop autopilot structure and incremental nonlinear dynamic inversion (INDI), providing new insights into nonlinear and adaptive control techniques. Furthermore, simulation results demonstrated that the proposed control loop can effectively estimate model uncertainties, offering good tracking performance even in the presence of model uncertainties.
목차
Abstract
I. 서론
II. 문제 정식화
III. 제안한 조종루프 알고리즘
IV. 수치 시뮬레이션
V. 결론
REFERENCES
참고문헌 (18)
참고문헌 신청
J. Jang, C. G. Jung, and C. H. Lee, “Technology Development Trends of Ultra-high-speed Target Wide Area Defense Systems,” Journal of Institute of Control, Robotics and Systems (in Korean), vol. 29, no. 3, pp. 20-29, 2023.
D. Schmidt, H. Mamich, and F. Chavez, “Dynamics and control of hypersonic vehicles-the integration challenge for the 1900’s,” The 3rd International Aerospace Planes Conference, 2012.
M. Mirmirani, C. Wu, A. Clark, S. B. Choi, and R. Colgren, “Modeling for control of a generic air-breathing hypersonic vehicle,” AIAA Guidance, Navigation, and Control Conference and Exhibit, 2005.
M. A. Bolender and D. B. Doman, “Nonlinear longitudinal dynamical model of an air-breathing hypersonic vehicle,” Journal of Spacecraft and Rockets, vol. 44, no. 2, pp. 374-387, 2007.
F. W. Nesline, B. H. Wells, and P. Zarchan, “A combined optimal/classical approach to robust missile autopilot design,” AIAA Guidance and Control Conference, AIAA Paper 1979-1731, 1979.
D. Schmidt, H. Mamich, and F. Chavez, “Dynamics and control of hypersonic vehicles-the integration challenge for the 1900’s,” The 3rd International Aerospace Planes Conference, 2012.
M. Mirmirani, C. Wu, A. Clark, S. B. Choi, and R. Colgren, “Modeling for control of a generic air-breathing hypersonic vehicle,” AIAA Guidance, Navigation, and Control Conference and Exhibit, 2005.
M. A. Bolender and D. B. Doman, “Nonlinear longitudinal dynamical model of an air-breathing hypersonic vehicle,” Journal of Spacecraft and Rockets, vol. 44, no. 2, pp. 374-387, 2007.
F. W. Nesline, B. H. Wells, and P. Zarchan, “A combined optimal/classical approach to robust missile autopilot design,” AIAA Guidance and Control Conference, AIAA Paper 1979-1731, 1979.
함께 읽어보면 좋을 논문
논문 유사도에 따라 DBpia 가 추천하는 논문입니다. 함께 보면 좋을 연관 논문을 확인해보세요!
-
Aircraft Control using Nonlinear Dynamic Inversion Based Control Law Designs
한국항공우주학회 학술발표회 초록집
2017 .11
-
Maneuverable Aircraft Flight Control Using Nonlinear Dynamic Inversion
제어로봇시스템학회 국제학술대회 논문집
2018 .10
-
Novel Unified Control Strategy for a Compound VTOL Vehicle
제어로봇시스템학회 국제학술대회 논문집
2024 .10
-
Lateral Mode Controller Design for Insect-like Tailless Flapping-Wing Micro Air Vehicle
제어로봇시스템학회 논문지
2021 .01
-
SIMULATION AND OPTIMIZATION METHODS OF THE THERMAL CONTROL LOOP OF SPACECRAFT
대한기계학회 춘추학술대회
2019 .05
-
기계임피던스 감소기법을 이용한 회전형 전기-유압식 구동기의 모델 없는 토크제어방법
로봇학회 논문지
2020 .03
-
Robust Output Voltage Tracking Control for Uncertain AC/DC Converter
제어로봇시스템학회 국제학술대회 논문집
2021 .10
-
극초음속 비행체의 3-루프 기반 비선형 비행경로각 제어기 설계
한국항공우주학회 학술발표회 초록집
2022 .11
-
Age of Information in Control Loop for Industrial IoT
한국정보과학회 학술발표논문집
2019 .06
-
Adaptive Sliding Mode Control of a Transport Aircraft for Heavyweight Airdrop
제어로봇시스템학회 국제학술대회 논문집
2015 .10
-
PDC Intelligent control-based theory for structure system dynamics
Smart Structures and Systems, An International Journal
2020 .01
-
The Effects of Maglev Chopper’s Control Cycle on Suspension Performance in EMS System
ICPE(ISPE)논문집
2019 .05
-
태양광패널 모사장치의 제어방식에 따른 소신호 특성 비교 분석
전력전자학회논문지
2021 .02
-
Control Capability : from Two-loop Autopilot to Three-loop Autopilot
제어로봇시스템학회 국제학술대회 논문집
2015 .10
-
ADAS 제어 성능 평가를 위한 Vehicle-in-the-Loop Simulation 환경 구축에 관한 연구
제어로봇시스템학회 국내학술대회 논문집
2019 .05
-
Fast locking All-Digital Phase-Locked Loop with Adaptive Loop Gain Control
한국통신학회 학술대회논문집
2019 .01
-
Stability Analysis and Optimal Control Design for Dual-Loop Voltage-Controlled Grid-Connected Inverters
ICPE(ISPE)논문집
2023 .05
-
Nonlinear Observer-based Control of Synchronous Machine Drive System
Journal of Electrical Engineering & Technology
2015 .05
-
비선형 동적 역변환 및 적응 추정기를 이용한 극초음속 비행체 종방향 제어기 설계
한국항공우주학회 학술발표회 초록집
2024 .11
-
Backstepping Controller Design of Maglev System for Air-gap Position Control
한국철도학회 논문집
2022 .03
이 논문의 저자 정보
이 논문과 함께 이용한 논문
극초음속 쐐기형 흡입구의 최대 전압력 회복률을 위한 오스와치 기법 분석
허엽
,
문규환
,
성홍계
한국항공우주학회지
2017
.12
항공기 비행기록장치에 대한 이해
김종현
항공진흥
2022
.12
무인 비행체의 PHM 기술 동향 및 발전 추세
김태균
,
김예지
,
이승신
외 1명
제어로봇시스템학회지
2024
.09
극초음속 비행체 복합엔진 Low Speed Flow Path 시제 설계 및 제작
강영석
,
이동은
,
이양지
외 2명
한국추진공학회 학술대회논문집
2024
.05
적 무인기 침투 비행경로 예측 모형
임영롱
,
이문걸
한국국방경영분석학회지
2024
.08
최근 본 자료
댓글(0)
0
UCI(KEPA) : I410-151-25-02-091208855