• Title/Summary/Keyword: Shipboard Landing

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Sea Wave Modeling Analysis and Simulation for Shipboard Landing of Tilt Rotor Unmanned Aerial Vehicle (틸트로터 무인기 함상이착륙 위한 파고운동 해석 및 시뮬레이션)

  • Yoo, Chang-Sun;Cho, Am;Park, Bum-Jin;Kang, Young-Shin
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.42 no.9
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    • pp.731-738
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    • 2014
  • The mission of UAV has been expanded from a land to an ocean based on an enhancement of its technologies. Korea Aerospace Research Institute (KARI) also tries to expand the mission of tilt rotor UAV to an ocean, in which the shipboard landing of UAV is required. However the environment of an oceanic operation is severer than that of land due to salty, fogy, and windy condition. The landing point for automatic landing is not fixed due to movement of shipboard in roll, pitch, and heave. It makes the oceanic operation and landing of UAV difficult. In order to conduct an oceanic operation of tilt rotor UAV, this paper presents that the sea wave modeling according to the sea state is conducted and the shipboard landing of tilt rotor UAV under the sea wave is tested and evaluated through the flight simulator for UAV.

Heave Motion Estimation of a Ship Deck for Shipboard Landing of a VTOL UAV (수직이착륙 무인기 함상 착륙점의 상하 운동 추정)

  • Cho, Am;Yoo, Changsun;Kang, Youngshin;Park, Bumjin
    • Journal of Aerospace System Engineering
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    • v.8 no.3
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    • pp.14-19
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    • 2014
  • When a helicopter lands on a ship deck in high sea states, one of main difficulties is the ship motion by sea wave, In case of a manned helicopter, a pilot lands a helicopter on the deck during quiescent period of ship motion, which is perceived from different visual cues around landing spot. The capability to predict this quiescent period is very important especially for shipboard recovery of VTOL UAV in harsh environments. This paper describes how to predict heave motion of a ship for shipboard landing of a VTOL UAV. For simulation, ship motion by sea wave was generated using a 4,000 ton class US destroyer model. Heave motion of ship deck was predicted by applying auto-regression method to generated time series data of ship motion.

Trade-Off Study of Shipboard Landing of Vertical Take-off and Landing Aircraft (수직이착륙 항공기의 함상이착륙 사례분석)

  • Yoo, Chang-Sun;Cho, Am;Park, Bun-Jin;Kang, Young-Shin
    • Aerospace Engineering and Technology
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    • v.12 no.1
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    • pp.10-21
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    • 2013
  • As helicopter technology has been upgraded, today its oceanic operation is considered to be usual. In oceanic operation of helicopter, the effect of severe wind, wave, and corrosion must be investigated and the operation procedures for safety as well as the motion of shipboard arising from maneuvers of ship must also be considered. In this paper, it describes the result of trade-off study for shipboard landing and its operation procedure including dynamic interface between ship and aircraft in ship operation and gives a simulation results to implement the oceanic operation of tilt rotor aircraft.

Development and Test of a Docking Type Automatic Landing System for Shipboard Landing (드론 함상 착륙을 위한 도킹 방식의 자동 착륙 시스템 개발 및 시험)

  • Minsu Park;Sungyug Kim;Hyeok Ryu
    • Journal of Aerospace System Engineering
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    • v.18 no.2
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    • pp.47-55
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    • 2024
  • The paper presents a docking-type automatic landing system that works in tandem with Unmanned Aerial Vehicles (UAVs) and Unmanned Surface Vehicles (USVs). The system utilizes a pyramid-shaped landing gear and pad for effective landing. In marine environments, a docking device guides the drone to land securely. To test the system, a ship's behavior was simulated using a 3-DoF motion platform, and the successful operation and utility of the docking-type automatic landing system were demonstrated.

Guidance and Control System Design for Automatic Carrier Landing of a UAV (무인 항공기의 함상 자동 착륙을 위한 유도제어 시스템 설계)

  • Koo, Soyeon;Lee, Dongwoo;Kim, Kijoon;Ra, Chung-Gil;Kim, Seungkeun;Suk, Jinyoung
    • Journal of Institute of Control, Robotics and Systems
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    • v.20 no.11
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    • pp.1085-1091
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    • 2014
  • This paper presents the guidance and control design for automatic carrier landing of a UAV (Unmanned Aerial Vehicle). Differently from automatic landing on a runway on the ground, the motion of a carrier deck is not fixed and affected by external factors such as ship movement and sea state. For this reason, robust guidance/control law is required for safe shipboard landing by taking the relative geometry between the UAV and the carrier deck into account. In this work, linear quadratic optimal controller and longitudinal/lateral trajectory tracking guidance algorithm are developed based on a linear UAV model. The feasibility of the proposed control scheme and guidance law for the carrier landing are verified via numerical simulations using X-Plane and Matlab/simulink.

Control Strategies for Landing Quadcopters on Ships with Legged Platform Based on Impedance Control (선박 위 착륙을 위한 임피던스 제어기반 쿼드콥터 족형 랜딩플랫폼 제어 전략)

  • Hwang, Seonghyeon;Lee, Seunghyeon;Jin, Seongho;Lee, Inho
    • The Journal of Korea Robotics Society
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    • v.17 no.1
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    • pp.48-57
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    • 2022
  • In this paper, we propose a legged landing platform for the quadcopter taking off and landing in the ship environment. In the ship environment with waves and winds, the aircraft has risks being overturned by contact impact and excessive inclination during landing on the ship. This landing platform has four landing legs under the quadcopter for balancing and shock relief. In order to make the quadcopter balanced on ships, the position of each end effector was controlled by PID control. And shocks have mainly happened when quadcopter contacts the ship's surface as well as legs move fast. Hence, impedance control was used to cope with the shocks. The performance of the landing platform was demonstrated by a simulation and a prototype in three sea states based on a specific size of a ship. During landing and tracking the slope of the ship's surface, oscillations of rotation and translation from the shock were mitigated by the controller. As a result, it was verified that transient response and stability got better by adding impedance control in simulation models and prototype experiments.