• 한국항해항만학회지
• /
• 제37권4호
• /
• pp.329-335
• /
• 2013

This paper is to develop the position error equations including the attitude errors, the errors of nadir and ship's heading, and the errors of ship's position in the free-gyro positioning and directional system. In doing so, the determination of ship's position by two free gyro vectors was discussed and the algorithmic design of the free-gyro positioning and directional system was introduced briefly. Next, the errors of transformation matrices of the gyro and body frames, i.e. attitude errors, were examined and the attitude equations were also derived. The perturbations of the errors of the nadir angle including ship's heading were investigated in each stage from the sensor of rate of motion of the spin axis to the nadir angle obtained. Finally, the perturbation error equations of ship's position used the nadir angles were derived in the form of a linear error model and the concept of FDOP was also suggested by using covariance of position error.

• 한국정밀공학회지
• /
• 제28권10호
• /
• pp.1181-1188
• /
• 2011

A control system for stabilizing a small robot or inverted pendulum using twisted gyro wheel is proposed. Conventional stabilizer using inertial wheel employs action-reaction force/torque to control a pendulum, which can generate relatively small torque and short period of output. In this paper, a novel actuation method using twisted gyro torque in 3-dimentional space was proposed to stabilizing a pendulum by twisting the assembly including a rotating gyro wheel. In addition, two special control functions for this type of twisted gyro wheel were designed. One is the function of self-adjusting the mass center of the robot and the other is the torque reloading configuration for continuous torque generation. The proposed system was verified by experimental result and simulation. The designed twisted gyro wheel control system can be easily packed in a small size module and installed in a humanoid robot or inverted pendulum type mechanism.

• 제어로봇시스템학회논문지
• /
• 제14권9호
• /
• pp.893-897
• /
• 2008

To achieve the challenges of low-cost MEMS gyros for the precise self-localization of mobile robots, this paper examines an effective method of minimizing the drift on the heading angle that relies solely on integration of rate signals from a gyro. The main idea of the proposed approach is to use wavelet de-noising filter in order to reduce random noise which affects short-term performances. The proposed method was applied to Epson XV3500 gyro and the performances are verified by the comparisons with an existing commercial gyro module of vacuum cleaning robots.

• Journal of Biosystems Engineering
• /
• 제23권2호
• /
• pp.179-186
• /
• 1998

This study was conducted to sense posture of an autonomous tractor using a DGPS, a gyro compass, and a potentiometer. Posture sensing system was constructed and its accuracy was evaluated. The accuracy of DGPS was evaluated under stationary and moving conditions, and the performance of the gyro compass and the potentiometer was investigated by measuring bearing and steering angles, respectively. Also, the effect of DGPS interference by obstacles was evaluated experimentally. The position accuracy was about 6.6cm(95%) under the stationary condition and 10 cm at sharp turning condition. Steering angle of the tractor could be related linearly to the output of the potentiometer that was installed on the rotating center of a knuckle arm. The positioning accuracy of the DGPS varied significantly according to the number of visible GPS satellites, but was good with more than 7 satellites. The DGPS gave bad solutions for sensing the posture of tractor when signals from satellites or the correction data from the base were interfered by obstacles.

• 한국항공우주학회지
• /
• 제34권9호
• /
• pp.97-103
• /
• 2006

본 논문에서는 디지털 폐루프 신호처리를 이용한 광섬유자이로를 설계하고 성능 시험한 결과를 제시하였다. 회전 입력에 대한 자이로의 피드백 제어를 위해 디지털 세로다인 변조기법이 적용되었고, 환산계수의 안정화를 위해 변조진폭 및 광전력 제어회로를 설계하였다. 프로토타입 광섬유자이로를 시험한 결과, 바이어스 안정도 0.34 deg/hr, 환산계수 비선형도약 100ppm , 회전감지 영역 ${\pm}500$ deg/sec의 성능을 얻었다.

• International Journal of Control, Automation, and Systems
• /
• 제4권3호
• /
• pp.351-358
• /
• 2006

The proposed inertial measurement unit (IMU) is composed of accelerometers only. It can determine a vehicle's position and attitude, which is the Gyro-free INS. The Gyro-free INS error is deeply affected by the sensor bias, scale factor and misalignment. However, these parameters can be obtained in the laboratory. After these misalignments are corrected, the Gyro-free strap-down INS could be more accurate. This paper presents a compensator design for the strap-down six-accelerometer INS to correct misalignment. A calibration experiment is taken to get the error parameters. A simulation results show that it will decrease the INS error to enhance the performance after compensation.

• 한국전자통신학회논문지
• /
• 제5권5호
• /
• pp.493-497
• /
• 2010

선박의 실시간 좌표변환 구현하였고, DC Servo Motor의 Motion Control 알고리즘을 개발하였다. Servo Control 회로설계 및 PCB를 제작하였고, 이를 3-axis Gyro Sensor based Servo Motion Control 제어장치에 적용하여 시스템을 개발하였다. 또한 선박운동을 시뮬레이터하기 위해서 6자유도를 가진 선박용 시뮬레이터를 개발하였다. 개발된 시뮬레이터에 장착된 카메라를 이용하여 선박운동을 추척하는 시험을 한 결과 원하는 오차내에서 추적결과를 보여주었다.

• 대한전자공학회논문지
• /
• 제26권4호
• /
• pp.1-6
• /
• 1989

본 논문은 gyro의drift에 관한 일반적 등가회로를 처음에 발진기의 위상안정을 규정화 하기 위하여 개발되었던 structure function 방법을 사용하여 분석하였다. 이 방법을 사용함으로서 임의의 order의 확정성, 내지 불확정성 성격의 Gyro drift가 쉽게 규정화되고 또 측정될 수 있음을 보였다. 그리고, drift의 power spectal density와 structure function과의 관계도 분명히 하였다. 마지막으로 이 방법을 이용하여 drift가 제어시스템에 끼치는 분석함이 매우 용이하게 됨을 보였다.

• Journal of Positioning, Navigation, and Timing
• /
• 제13권2호
• /
• pp.179-187
• /
• 2024

The performance of a Strapdown Inertial Navigation System (SDINS) relies heavily on the accuracy of sensor error calibration. Systematic calibration is usually employed when only a 2-axis turntable is available. For systematic calibration, the body frame is commonly defined with respect to sensor axes for ease of computation. The drawback of this approach is that sensor axes may undergo time-varying deflection under temperature change, causing pseudo gyro bias. The effect of pseudo gyro bias on navigation performance is negligible for low grade navigation systems. However, for higher grade systems undergoing rapid temperature change, the error is no longer negligible. This paper describes in detail conditions leading to the presence of pseudo gyro bias, and proposes two techniques for mitigating the error. Experimental results show that applying these techniques improves navigation performance for precision SDINS, especially under rapid temperature change.

• Journal of Astronomy and Space Sciences
• /
• 제22권2호
• /
• pp.175-186
• /
• 2005

본 논문에서는 정지궤도 통신위성인 무궁화위성 3호 버스 시스템을 모델로 하여 확장칼만필터를 이용한 자세결정 알고리즘을 개발하고 그 설계 결과를 시뮬레이션을 통해 제시하였다. 특히, 정확한 추정을 위한 칼만필터의 필터 이득을 결정하기 위해서는 초기에 입력된 추정변수들의 값에 변동이 없는 상황을 가정하게 되는데 본 연구에서는 2Hz 로 자세제어도 동시에 수행하면서 필터이득을 구하여 추정변수들의 값에 변동이 있는 상황에서도 필터가 정상적으로 동작됨을 보였다. 최종적으로 필터를 사용하지 않은 경우와 사용한 경우를 고려하여 4축 자이로의 각 바이어스가 있는 경우 및 개별적으로 자이로가 고장이 난 경우의 시뮬레이션 결과를 통해 설계된 필터가 자이로 이상상태를 대처할 수 있음을 검증하였다.