• Title/Summary/Keyword: Earth Fixed Earth Centered Coordinate

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Precision Coordinate Transformation and Gravity Acceleration Algorithms (정밀좌표변환 및 중력가속도 계산 알고리듬 분석)

  • Kim, Jeong-Rae;Noh, Jeong-Ho
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.19 no.4
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    • pp.30-36
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    • 2011
  • Inertial navigation systems requires gravity model to compute gravity acceleration and its trajectory accuracy depends on the gravity model accuracy especially for a long range flight. The gravity model accuracy is important for satellite orbit prediction as well. The precision gravity model requires a precision coordinate transformation between inertial and Earth fixed coordinates. Precision gravity acceleration algorithms with a coordinate transform are studied and a computer program is developed. The effects of individual model components on trajectory error are analyzed.

A Study on the GEO-Tracking Algorithm of EOTS for the Construction of HILS system (HILS 시스템 구축을 위한 EOTS의 좌표지향 알고리즘 실험에 대한 연구)

  • Gyu-Chan Lee;Jeong-Won Kim;Dong-Gi Kwag
    • The Journal of the Convergence on Culture Technology
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    • v.9 no.1
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    • pp.663-668
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    • 2023
  • Recently it is very important to collect information such as enemy positions and facilities. To this end, unmanned aerial vehicles such as multicopters have been actively developed, and various mission equipment mounted on unmanned aerial vehicles have also been developed. The coordinate-oriented algorithm refers to an algorithm that calculates a gaze angle so that the mission equipment can fix the gaze at a desired coordinate or position. Flight data and GPS data were collected and simulated using Matlab for coordinate-oriented algorithms. In the simulation using only the coordinate data, the average Pan axis angle was about 0.42°, the Tilt axis was 0.003°~0.43°, and the relatively wide error was about 0.15° on average. As a result of converting this into the distance in the NE direction, the error distance in the N direction was about 2.23m on average, and the error distance in the E direction was about -1.22m on average. The simulation applying the actual flight data showed a result of about 19m@CEP. Therefore, we conducted a study on the self-error of coordinate-oriented algorithms in monitoring and information collection, which is the main task of EOTS, and confirmed that the quantitative target of 500m is satisfied with 30m@CEP, and showed that the desired coordinates can be directed.