• Title/Summary/Keyword: 회전형 관성 항법 시스템

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Stabilization Technique for a Dual-axis Rotational Inertial Navigation System considering Waves (파도를 고려한 2축 회전형 관성항법시스템의 안정화 기법)

  • Myeong-Seok Chae;Seong-Yun Cho;Chan-Gook Park;Min-Su Jo;Chan-Joo Park
    • The Journal of the Korea institute of electronic communication sciences
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    • v.19 no.2
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    • pp.437-444
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    • 2024
  • The rotational inertial navigation system can provide more accurate navigation information by mounting an IMU (Inertial Measurement Unit) on the gimbal and rotating the gimbal regularly to cancel out the errors of the IMU. However, when an attitude change occurs due to waves, the attitude error is not removed to 0 at the end of one cycle of the rotation procedure and causes a large position error. In this paper, considering this problem, we propose a method of stabilizing the external gimbal by rotating it based on the roll information of the vehicle. Based on simulation, the impact of waves is analyzed and the performance of external gimbal stabilization is verified.

Development of Flight Control System for Gliding Guided Artillery Munition - Part I : Operational Concept and Navigation (유도형 활공 탄약 비행제어시스템 개발 Part I : 운용 개념 및 항법)

  • Lim, Seunghan;Pak, Changho;Cho, Changyeon;Bang, Hyochoong
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.42 no.3
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    • pp.221-228
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    • 2014
  • In this paper, the operational concept and the navigation algorithms for the gliding guided artillery munition are studied. The gliding guided artillery munition has wings for gliding; therefore spin of the munition should be eliminated. The previous navigation algorithms assumed a spinning munition with constant angular velocity; hence, they cannot be applied for the gliding munition. Moreover, lateral stability becomes worse due to decrease of angular momentum. Therefore, side force should be controlled to improve the stability, and the munition should maneuver, then the previous navigation algorithms for typical fixed-wing aircraft cannot be applied. In this paper, we apply the previous navigation algorithms for the spinning munition. Spin is eliminated and wings are deployed based on the estimation results, and the advanced navigation algorithm for the non-spinning munition is introduced.

Implementation of an Intelligent Automatic Parking Assist System (지능형 자동 주차 지원 시스템의 구현)

  • Park Cheong-Sool;Han Min-Hong
    • Journal of the Institute of Convergence Signal Processing
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    • v.6 no.4
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    • pp.182-190
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    • 2005
  • In the paper, we propose an intelligent automatic parking assist system. To realize an automatic parking, first, the prospective parking position and the location of a vehicle should be recognized. Second, the system should compute a path which introduces the parking position precisely with avoiding any obstacles. Third, the handle should be controlled so that the vehicle moves through the path. To calculate the location of the vehicle and its surroundings, the system applies the camera image method to transforming input images to the plane map. It also uses the inertial navigation method which recognizes the position and the direction of a moving vehicle by using a kinematic model of the vehicle. To generate a path of the vehicle, the simple path method and the Bezier spline method are tested. The divided arc method which generates multiple paths is also tested. We apply a method which makes the system choose the best path with multiple objective functions. We introduce the virtual road method, as a solution for the problem of mechanical time delay, to have the vehicle followed the designated path.

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