• 제목/요약/키워드: roll and pitch angle

검색결과 122건 처리시간 0.022초

농업 로봇 용 수평 자세 모니터링 시스템 개발 (Development of Horizontal Attitude Monitoring System for Agricultural Robots)

  • 김성득;김청월;권익현;이영태
    • 반도체디스플레이기술학회지
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    • 제18권2호
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    • pp.87-91
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    • 2019
  • In this paper, we have development of horizontal attitude monitoring system for agricultural robots. A two-axis gyro sensor and a two-axis accelerometer sensor are used to measure the horizontal attitude angle. The roll angle and pitch angle were measured through the fusion of the gyro sensor signal and the acceleration sensor signal for the horizontal attitude monitoring of the robot. This attitude monitoring system includes GPS and Bluetooth communication module for remote monitoring. The roll angle and pitch angle can be measured by the error of less than 1 degree and the linearity and the reproducibility of the output signal are excellent.

정상 임무운용 상태에서 다목적실용위성 2호 탑재체에 대한 태양 입사각 분석 (SUN INCIDENCE ANGLE ANALYSIS OF KOMPSTAT-2 PAYLOAD DURING NORMAL MISSION OPERATIONS)

  • 김응현;용기력;이상률
    • Journal of Astronomy and Space Sciences
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    • 제17권2호
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    • pp.309-316
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    • 2000
  • KOMPSAT-2 will carry MSC(Multi-Spectral Camera) which provides 1m resolution panchromatic and 4m resolution multi-spectral images at the altitude of 685km sun-synchronous mission orbit. The mission operation of KOMSPAT-2 is to provide the earth observation using MSC with nadir pointing. KOMPSAT-2 will also have the capability of roll/pitch tilt maneuver using reaction wheel of satellite as required. In order to protect MSC from thermal distortion as well as direct sunlight, MSC shall be operated within the constraint of sun incidence angle. It is expected that the sunlight will not violate the constraint of sun incidence angle for normal mission operations without roll/pitch maneuver. However, during roll/pitch tilt operations, optical module of MSC may be damaged by the sunlight. This study analyzed sun incidence angle of payload using KOMPSAT-2 AOCS (Attitude and Orbit Control Subsystem) Design and Performance Analysis Soft ware for KOMPSAT-2 normal mission operations.

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Roll-Pitch-Yaw Integrated H Controller Synthesis for High Angle-of-Attack Missiles

  • Choi, Byung-Hun;Kang, Seon-Hyeok;Kim, H. Jin;Won, Dae-Yeon;Kim, Youn-Hwan;Jun, Byung-Eul;Lee, Jin-Ik
    • International Journal of Aeronautical and Space Sciences
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    • 제9권1호
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    • pp.66-75
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    • 2008
  • In this work, we explore the feasibility of roll-pitch-yaw integrated autopilots for high angle-of-attack missiles. An investigation of the aerodynamic characteristics of a surface-to-air missile is presented, which reveals the strong effects of cross coupling between the longitudinal and lateral dynamics. Robust control techniques based on $H_{\infty}$ synthesis are employed to design roll-pitch-yaw integrated autopilots. The performance of the proposed roll-pitch-yaw integrated controller is tested in high-fidelity nonlinear five-degree-of-freedom simulations accounting for kinematic cross-coupling effects between the lateral and longitudinal channels. Against nonlinearity and cross-coupling effects of the missile dynamics, the integrated controller demonstrates superior performance when compared with the controller designed in a decoupled manner.

세기변조방사선치료에서 Pitch와 Roll 변화에 따른 선량전달 정확성 평가 (Evaluation of dose delivery accuracy due to variation in pitch and roll)

  • 정창영;배선명;이동형;민순기;강태영;백금문
    • 대한방사선치료학회지
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    • 제26권2호
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    • pp.239-245
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    • 2014
  • 목 적 : 세기변조방사선치료에서(Intensity modulated radiation therapy,IMRT) 6D robotic couch의 pitch 와 roll 변화에 따른 선량전달의 정확성을 평가하고자 한다. 대상 및 방법 : Trilogy(Varian Medical Systems, USA)와 6D robotic couch(ProturaTM 1.4, CIVCO, USA)를 사용하여 골반부위의 세기변조방사선치료를 진행한 14명의 환자를 대상으로 영상유도 시 발생한 pitch 와 roll 방향의 오차 값과 발생빈도를 분석하였다. 오차의 변화에 따른 선량전달 정확성의 차이를 평가하기 위해 pitch 와 roll의 변화가 $0^{\circ}$인 상태의 측정치를 기준으로 각각 $1.0^{\circ}$, $1.5^{\circ}$, $2.0^{\circ}$, $2.5^{\circ}$로 변화시킨 경우에 대하여 2차원 이온전리함 배열 검출기(I'mRT Matrixx, IBA Dosimetry,Germany)와 MultiCube Phantom(IBA Dosimetry, Germany)를 이용하여 측정 후 감마지수(3 mm, 3%)의 비교평가를 실시하였다. 실험에는 Dynamic Multi-Leaf Collimator의 sliding window기법을 사용한 3명의 자궁경부암 치료계획을 적용하였다. 결 과 : 대상 환자의 영상(3D/3D Match 78건, 2D/2D match 79건)을 분석한 결과 pitch 와 roll의 평균 오차값은 $0.9^{\circ}{\pm}0.7$, $0.5^{\circ}{\pm}0.6$, 최대 값은 $2.8^{\circ}$, $2.0^{\circ}$로 분석되었고, 최소값은 pitch 와 roll 모두 $0^{\circ}$으로 나타났다. 각각의 조건에서 측정된 선량전달에 대하여 감마지수를 이용하여 비교한 결과, pitch가 $1.0^{\circ}$, $1.5^{\circ}$, $2.0^{\circ}$, $2.5^{\circ}$일 때 gamma pass rate의 평균은 각각 97.75%, 96.65%, 94.38%, 90.91%, roll의 경우 $1.0^{\circ}$, $1.5^{\circ}$, $2.0^{\circ}$, $2.5^{\circ}$에서 평균 93.68%, 93.05%, 87.77%, 84.96%로 나타났고, pitch 와 roll을 동시에 변화시킨 경우 $1.0^{\circ}$, $1.5^{\circ}$, $2.0^{\circ}$에서 평균 94.90%, 92.37%, 87.88%의 결과 값을 얻었다. 결 론 : 대상 환자의 영상 유도 시 pitch 와 roll의 오차 발생률은 전체 치료 횟수에서 각각 82.20%, 72.20%로 분석되었고, 감마지수를 통해 오차 값이 커질수록 선량전달의 정확성이 낮아진다는 것을 확인할 수 있었다. 세기변조방사선치료 시 선량전달의 정확성을 높이기 위해서는 정확한 자세잡이와 더블어 적절한 영상유도를 통해서 pitch 와 roll 방향으로 발생할 수 있는 오차를 줄이도록 노력해야 할 것으로 사료된다.

연속회전을 통한 능동 합성개구레이더위성 기동시간 단축 연구 (A Study on Active SAR Satellite Maneuver Time Reduction through Sequential Rotation)

  • 손준원;박영웅
    • 한국항공우주학회지
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    • 제43권7호
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    • pp.648-656
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    • 2015
  • 능동 합성개구레이더 위성의 주요기동은 SAR 안테나 방향을 바꾸기 위한 롤축 기동이다. 그리고 도플러 중심주파수 변화를 최소화하기 위하여 요축 기동이 요구된다. 따라서 토크/모멘텀 용량을 대부분 롤축으로 그 다음으로 요축으로 할당하는 것이 합리적이다. 하지만 궤도 조정 때문에 가끔씩 피치축으로 중심으로 큰 각도의 회전이 요구된다. 본 논문에서는 롤축과 요축의 연속회전을 통한 피치축 기동시간 단축 방법에 대해서 살펴본다. 이들 두 축이 피치축에 비해서 기동성능이 좋기 때문에, 피치축을 중심으로 큰 회전이 요구될 때는 기동시간 단축이 가능하다.

Optimization of ride comfort for a three-axle vehicle equipped with interconnected hydro-pneumatic suspension system

  • Saglam, Ferhat;Unlusoy, Y. Samim
    • Advances in Automotive Engineering
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    • 제1권1호
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    • pp.1-20
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    • 2018
  • The aim of this study is the optimization of the parameters of interconnected Hydro-Pneumatic (HP) suspension system of a three-axle vehicle for ride comfort and handling. For HP suspension systems of equivalent vertical stiffness and damping characteristics, interconnected HP suspension systems increase roll and pitch stiffness and damping characteristics of the vehicle as compared to unconnected HP suspension systems. Thus, they result in improved handling and braking/acceleration performances of the vehicle. However, increased roll and pitch stiffness and damping characteristics also increase roll and pitch accelerations, which in turn result in degraded ride comfort performance. Therefore, in order to improve both ride comfort and vehicle handling performances simultaneously, an optimum parameter set of an interconnected HP suspension system is obtained through an optimization procedure. The objective function is formed as the sum of the weighted vertical accelerations according to ISO 2631. The roll angle, one of the important measures of vehicle handling and driving safety, is imposed as a constraint in the optimization study. Upper and lower parameter bounds are used in the optimization in order to get a physically realizable parameter set. Optimization procedure is implemented for a three-axle vehicle with unconnected and interconnected suspension systems separately. Optimization results show that interconnected HP suspension system results in improvements in both ride comfort and vehicle handling performance, as compared to the unconnected suspension system. As a result, interconnected HP suspension systems present a solution to the conflict between ride comfort and vehicle handling which is present in unconnected suspension systems.

스트랩다운 관성항법시스템의 초기 개략정렬 알고리즘 (An initial coarse alignment algorithm for strapdown inertial navigation system)

  • 박찬국;김광진;이장규
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 1996년도 한국자동제어학술회의논문집(국내학술편); 포항공과대학교, 포항; 24-26 Oct. 1996
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    • pp.856-859
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    • 1996
  • In this paper, a coarse alignment algorithm for strapdown inertial navigation system is proposed and evaluated analytically. The algorithm computes roll and pitch angles of the vehicle using accelerometer outputs, and then determines yaw angle with gyro outputs. It is referred, as two-step coarse alignment in this work. With the geometric relation between sensor outputs and roll, pitch and yaw angles, the algorithm error is analytically derived and compared with the previous coarse alignment algorithm introduced by Britting. The results show that the proposed two-step coarse alignment algorithm has better performance for pitch angle computation.

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무궁화 방송통신 위성의 3축 자세 안정화 장치에 관한 연구 (A study on the 3-axis attitude stabilization of Koreasat)

  • 진익민;백명진;김진철
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 1993년도 한국자동제어학술회의논문집(국내학술편); Seoul National University, Seoul; 20-22 Oct. 1993
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    • pp.793-798
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    • 1993
  • In this study the attitude control of the KOREASAT is investigated. The KOREASAT is a geostationary satellite and its 3 attitude angles, namely, roll, pitch and yaw angles, are stabilized by using the 3-axis stabilization technique. In the pitch control loop, the pitch attitude angle received from the earth sensor is processed in the attitude processing electronics by using PI type control logic, and the control command is sent to the momentum wheel assembly to generate the control torque by varying the wheel rate. The roll/yaw attitude control is performed by activating a magnetic torquer or by firing appropriate thrusters. The magnetic torquer interacts with the earth magnetic field to produce the control torque, and the thrusters are used to control the larger roll attitude errors. In this study dynamic modelling of the satellite is performed. And the earth sensor, the momentum wheel, and the magnetic torquer are mathematically modelled. The 3-axis attitude control logic is implemented to make the closed-loop system and simulations are carried out to verify the implemented control laws.

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Integrated Roll-Pitch-Yaw Autopilot via Equivalent Based Sliding Mode Control for Uncertain Nonlinear Time-Varying Missile

  • AWAD, Ahmed;WANG, Haoping
    • International Journal of Aeronautical and Space Sciences
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    • 제18권4호
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    • pp.688-696
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    • 2017
  • This paper presents an integrated roll-pitch-yaw autopilot using an equivalent based sliding mode control for skid-to-turn nonlinear time-varying missile system with lumped disturbances in its six-equations of motion. The considered missile model are developed to integrate the model uncertainties, external disturbances, and parameters perturbation as lumped disturbances. Moreover, it considers the coupling effect between channels, the variation of missile velocity and parameters, and the aerodynamics nonlinearity. The presented approach is employed to achieve a good tracking performance with robustness in all missile channels simultaneously during the entire flight envelope without demand of accurate modeling or output derivative to avoid the noise existence in the real missile system. The proposed autopilot consisting of a two-loop structure, controls pitch and yaw accelerations, and stabilizes the roll angle simultaneously. The Closed loop stability is studied. Numerical simulation is provided to evaluate performance of the suggested autopilot and to compare it with an existing autopilot in the literature concerning the robustness against the lumped disturbances, and the aforesaid considerations. Finally, the proposed autopilot is integrated in a six degree of freedom flight simulation model to evaluate it with several target scenarios, and the results are shown.

퍼지-슬라이딩모드 제어기를 이용한 외바퀴 로봇의 자세제어 및 방향제어 (Attitude and Direction Control of the Unicycle Robot Using Fuzzy-Sliding Mode Control)

  • 이재오;한성익;한인우;이석인;이장명
    • 제어로봇시스템학회논문지
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    • 제18권3호
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    • pp.275-284
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    • 2012
  • This paper proposes an attitude and direction control of a single wheel balanced robot. A unicycle robot is controlled by two independent control laws: the mobile inverted pendulum control method for pitch axis and the reaction wheel pendulum control method for roll axis. It is assumed that both roll dynamics and pitch dynamics are decoupled. Therefore the roll and pitch dynamics are obtained independently considering the interaction as disturbances to each other. Each control law is implemented by a controller separately. The unicycle robot has two DC motors to drive the disk for roll and to drive the wheel for pitch. Since there is no force to change the yaw direction, the present paper proposes a method for changing the yaw direction. The angle data are obtained by a fusion of a gyro sensor and an accelerometer. Experimental results show the performance of the controller and verify the effectiveness of the proposed control algorithm.