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Proceedings Paper

The verification of UAV's autopilot system with realtime HILS
Author(s): Min-Soo Kim; Hyeong-Jik Kong; Soo-Ho Baek; Yu-Hwan Choe; Sung-Kyung Hong
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Paper Abstract

Unmanned aerial vehicle (UAV) was designed to fulfill its mission autonomously. Its core technology for successful development of the UAV is to design of the flight control system (FCS) consisting of the flight control computer, the actuator, the sensor in order to replace the pilot. Each development procedure of FCS involves a verifying test for each step and was completed by an evaluation test of the comprehensive performance verification for the overall systems. The development tool, which is applied to this objective, is the HILS (Hardware-In-the-Loop-Simulation). That is, HILS is a cost-effective method for testing complex, flight-critical hardware before it is used in the real world. The real-time HILS is shown to develop/verify the performance of SURV UAV's controller in the lateral/directional control systems.

Paper Details

Date Published: 2 May 2006
PDF: 6 pages
Proc. SPIE 6042, ICMIT 2005: Control Systems and Robotics, 60422I (2 May 2006); doi: 10.1117/12.664661
Show Author Affiliations
Min-Soo Kim, Sejong-Lockheed Martin Aerospace Research Ctr. (South Korea)
Hyeong-Jik Kong, Sejong Univ. (South Korea)
Soo-Ho Baek, Sejong Univ. (South Korea)
Yu-Hwan Choe, Sejong Univ. (South Korea)
Sung-Kyung Hong, Sejong Univ. (South Korea)


Published in SPIE Proceedings Vol. 6042:
ICMIT 2005: Control Systems and Robotics

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