• Title/Summary/Keyword: Attitude Tracking

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Adaptive Backstepping Hovering Control for a Quadrotor with Unknown Parameters (미지 파라미터를 갖는 쿼드로터의 적응 백스테핑 호버링 제어)

  • Lee, Keun Uk;Park, Jin Bae;Choi, Yoon Ho
    • Journal of Institute of Control, Robotics and Systems
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    • v.20 no.10
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    • pp.1002-1007
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    • 2014
  • This paper deals with the adaptive backstepping hovering control for a quadrotor with model parameter uncertainties. In this paper, the backstepping based technique is utilized to design a nonlinear adaptive controller which can compensate for the motor thrust factor and the drag coefficient of a quadrotor. First, the quadrotor nonlinear dynamics is derived using Newton-Euler formulation. In particular, we use the ${\pi}/4$ shifted coordinate for x- and y-axis of a quadrotor. Second, an adaptive backstepping based attitude and altitude tracking control method is presented. The system stability and the convergence of tracking errors are proven using the Lyapunov stability theory. Finally, the simulation results are given to verify the effectiveness of the proposed control method.

Non-regressor Based Adaptive Tracking Control of an Underwater Vehicle-mounted Manipulator (수중 선체에 장착된 로봇팔 궤적의 비귀환형 적응제어)

  • 여준구
    • Journal of Ocean Engineering and Technology
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    • v.14 no.2
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    • pp.7-12
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    • 2000
  • This paper presents a non-regressor based adaptive control scheme for the trajectory tracking of underwater vehicle-mounted manipulator systems(UVMS). The adaptive control system includes a class of unmodeled effects is applied to the trajectory control of an UVMS. The only information required to implement this scheme ios the upper bound and lowe bound of the system parameter matrices the upper bound of unmodeled effects the number of joints the position and attitude of the vehicle and trajectory commands. The adaptive control law estimates control gains defined by the combinations of the bounded constants of system parameter matrices and of a filtered error equation. To evaluate the performance of the non-regressor based adaptive controller computer simulation was performed with a two-link planar robot model mounted on an underwater vehicle. The hydrodynamic effects acting on the manipulator are included. It is assumed that the vehicle's motion is slow and can be predicted with a proper compensator.

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Robust Waypoint Tracking of Large Diameter Unmanned Underwater Vehicles with Uncertain Hydrodynamic Coefficients (불확실 유체 역학 계수를 가진 대형급 무인잠수정의 강인 경로점 추적)

  • Kim, Do Wan;Park, Jeong-Hoon;Park, Ho-Gyu;Kim, Tae-Yeong
    • The Transactions of The Korean Institute of Electrical Engineers
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    • v.66 no.2
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    • pp.409-415
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    • 2017
  • This paper addresses on an linear matrix inequality (LMI) formulation of the robust waypoint tracking problem of large diameter unmanned underwater vehicles (LDUUVs) in the horizontal plane. The interested design issue can be reformed as the robust asymptotic stabilization of the provided error dynamics with respect to the desired yaw angle, surge speed and attitude. Sufficient conditions for its robust asymptotic stabilizability against the hydrodynamic uncertainties are derived in the format of LMI. An example is provided to testify the validity of the proposed theoretical claims.

Study on Analyzing and Correction of Dynamic Battery Alignment Error in Naval Gun Fire Control System by using Image of Boresight Telescope (포배열카메라 영상을 활용한 함포 사격통제시스템의 동적배열오차 분석 및 보정방법)

  • Kim, Eui-Jin;Suh, Tae Il
    • Journal of the Korea Institute of Military Science and Technology
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    • v.16 no.6
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    • pp.745-751
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    • 2013
  • In naval gun firing, firing accuracy comes from the combination of each component's accuracy in CFCS (Command and Fire Control System) like tracking sensors and gun. Generally, battery alignment is done to correct the error between gun and tracking sensor by using boresight telescope on harbor and sea. But normally, the battery alignment can compensate only the static alignment error and ignore dynamic alignment error which is caused by own ship movement. There was no research on this dynamic alignment error until now. We propose a new way to analyze dynamic arrangement error by using image of boresight telescope. In case of the dynamic alignment error was due to time delay of own ship attitude information, we propose the way to compensate it.

Precise Braking Torque Control for Momentum Flywheels Based on a Singular Perturbation Analysis

  • Zhou, Xinxiu;Su, Dan
    • Journal of Power Electronics
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    • v.17 no.4
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    • pp.953-962
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    • 2017
  • Momentum flywheels are widely applied for the generation of small and precise torque for the attitude control and inertial stabilization of satellites and space stations. Due to its inherited system nonlinearity, the tracking performance of the flywheel torque/speed in dynamic/plug braking operations is limited when a conventional controller is employed. To take advantage of the well-separated two-time-scale quantities of a flywheel driving system, the singular perturbation technique is adopted to improve the torque tracking performance. In addition, the composite control law, which combines slow- and fast- dynamic portions, is derived for flywheel driving systems. Furthermore, a novel control strategy for plug braking dynamics, which considers couplings between the Buck converter and the three-phase inverter load, is designed with easy implementation. Finally, experimental results are presented to demonstrate the correctness of the analysis and the superiority of the proposed methods.

Trajectory Tracking Control for Two Wheeled Mobile Robot using Fuzzy Sliding Mode Control based Hyperbolic Function (하이퍼볼릭 함수 기반의 퍼지 슬라이딩 모드 제어를 이용한 2바퀴 이동로봇의 경로 추종제어)

  • Lim, Jong-Uk;Lee, Sang-Jae;Chai, Chang-Hyun
    • Journal of the Korean Society of Manufacturing Process Engineers
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    • v.13 no.3
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    • pp.28-34
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    • 2014
  • In this paper, we propose a trajectory tracking controller for a two-wheeled mobile robot (WMR) with nonholonomic constraints using a fuzzy sliding-mode controller-based hyperbolic function. The proposed controller is composed of two separate controllers. The sliding-mode controller is used for attitude control of the WMR, and the fuzzy controller-based hyperbolic function is designed to adjust the reach time of the sliding-mode control. Simulation results on a linear and a circular trajectory show that the proposed controller improves the control performance. The proposed controller reduces the reach time by as much as 47% compared to the controller proposed by Xie et al.

Development of Sensor Device and Probability-based Algorithm for Braille-block Tracking (확률론에 기반한 점자블록 추종 알고리즘 및 센서장치의 개발)

  • Roh, Chi-Won;Lee, Sung-Ha;Kang, Sung-Chul;Hong, Suk-Kyo
    • Journal of Institute of Control, Robotics and Systems
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    • v.13 no.3
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    • pp.249-255
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    • 2007
  • Under the situation of a fire, it is difficult for a rescue robot to use sensors such as vision sensor, ultrasonic sensor or laser distance sensor because of diffusion, refraction or block of light and sound by dense smoke. But, braille blocks that are installed for the visaully impaired at public places such as subway stations can be used as a map for autonomous mobile robot's localization and navigation. In this paper, we developed a laser sensor stan device which can detect braille blcoks in spite of dense smoke and integrated the device to the robot developed to carry out rescue mission in various hazardous disaster areas at KIST. We implemented MCL algorithm for robot's attitude estimation according to the scanned data and transformed a braille block map to a topological map and designed a nonlinear path tracking controller for autonomous navigation. From various simulations and experiments, we could verify that the developed laser sensor device and the proposed localization method are effective to autonomous tracking of braille blocks and the autonomous navigation robot system can be used for rescue under fire.

Error Correction of Interested Points Tracking for Improving Registration Accuracy of Aerial Image Sequences (항공연속영상 등록 정확도 향상을 위한 특징점추적 오류검정)

  • Sukhee, Ochirbat;Yoo, Hwan-Hee
    • Journal of Korean Society for Geospatial Information Science
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    • v.18 no.2
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    • pp.93-97
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    • 2010
  • This paper presents the improved KLT(Kanade-Lucas-Tomasi) of registration of Image sequence captured by camera mounted on unmanned helicopter assuming without camera attitude information. It consists of following procedures for the proposed image registration. The initial interested points are detected by characteristic curve matching via dynamic programming which has been used for detecting and tracking corner points thorough image sequence. Outliers of tracked points are then removed by using Random Sample And Consensus(RANSAC) robust estimation and all remained corner points are classified as inliers by homography algorithm. The rectified images are then resampled by bilinear interpolation. Experiment shows that our method can make the suitable registration of image sequence with large motion.

Autonomous Landing on Small Bodies based on Discrete Sliding Mode Control (이산 슬라이딩 모드 제어를 이용한 소천체 자율 착륙 기법)

  • Lee, Juyoung
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.45 no.8
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    • pp.647-661
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    • 2017
  • This paper presents a robust method for autonomously landing on small bodies. Autonomous landing is accomplished by generating and following reference position and attitude profiles. The position and attitude tracking controllers are based on discrete sliding mode control, which explicitly treats the discrete and impulsive natures of thruster operation. Vision-based inertial navigation is used for autonomous navigation for landing. Numerical simulation is carried out to evaluate the performance of the proposed method in a realistic situation with environmental uncertainties.

Tiltrotor Attitude Control Using L1 Adaptive Controller (L1 적응제어기법을 이용한 틸트로터기의 자세제어)

  • Kim, Nak-Wan;Kim, Byoung-Soo;Yoo, Chang-Sun;Kang, Young-Sin
    • Journal of Institute of Control, Robotics and Systems
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    • v.14 no.12
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    • pp.1226-1231
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    • 2008
  • A design of attitude controller for a tiltrotor is presented augmenting L1 adaptive control, neural networks, and feedback linearization. The neural networks compensate for the modeling error caused by the lack of knowledge of tiltrotor dynamics while the L1 adaptive control allows high adaptation gains in adaptation laws thereby, satisfying tracking performance requirement. The efficacy of this control methodology is illustrated in high-fidelity nonlinear simulation of a tiltrotor by flying the tiltrotor in different flight modes from where the L1 adaptive controller with neural networks is originally designed for.