Výsledky vyhledávání - "Heung-Sik Lim"

Design and Integration of a Dual Redundancy Air Data System for Unmanned Air Vehicles

Autor: Hongju Lee, Taekyeum Kim, Jin-Sung Hong, Seonghun Yun, Sun-yu Hwang, Dae-Yeon Won, Heung-Sik Lim

Publikováno v: Journal of the Korea Institute of Military Science and Technology. 23:639-649

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::4555200a1f109cc54d4c68dc6c54fd05
https://doi.org/10.9766/kimst.2020.23.6.639

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Analysis of partial wing damage on flying-wing unmanned air vehicle

Autor: Seungkeun Kim, Gi-bong Hur, Jong-Soo Choi, Jong-Min Ahn, Jinyoung Suk, Heung-Sik Lim, Kijoon Kim

Publikováno v: Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. 228:355-374

This article investigates the effect of asymmetric wing damage on flight dynamic characteristics of a flying-wing single motor unmanned air vehicle. To construct a six degree-of-freedom model of the damaged aircraft, a flying-wing type unmanned aeria

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::75cd991f4d91a25ec9bb3122f8e26543
https://doi.org/10.1177/0954410012472292

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Development of Guidance Control Module for GPS Guided Bomb

Autor: Heung-Sik Lim, Hyung-Sik Yoon

Publikováno v: Journal of the Korea Institute of Military Science and Technology. 14:774-780

The guidance control module is needed for control of a GPS guided bombs to improve the accuracy and availability of a conventional bomb. In this paper, we present the development of hardware design, software design and test environments of it. And we

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::79e15494c6598e89befadd55662a0ef9
https://doi.org/10.9766/kimst.2011.14.5.774

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Development of Operational Flight Program for Avionic System Computer

Autor: Sung Soo Lee, Young Il Kim, Heung-Sik Lim, Sang-Hwan Kim

Publikováno v: Journal of the Korean Society for Aeronautical & Space Sciences. 33:104-112

This paper presents the technique to develop an operational flight program(OFP) of avionic system computer(ASC) which integrates the avionics control, navigation and fire control and provides informations for flight, navigation and weapon aiming miss

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::0e1a89a0e73d8cad1ada61baa8baf8e2
https://doi.org/10.5139/jksas.2005.33.9.104

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Flight test of a Flying-Wing Type UAV with Partial Wing Loss Using Neural Network Controller

Autor: Gi-bong Hur, Kijoon Kim, Do-Myung Kim, Heung-Sik Lim, Nakwan Kim, Jong-Min Ahn, Seungkeun Kim, Jinyoung Suk, Byoung Soo Kim

Publikováno v: Scopus-Elsevier

This paper presents flight test result of flying-wing type UAV with partial wing loss using neural network controller. 22% and 33% loss of wing area moment were considered for the damage configuration. A new trim state was obtained for each damaged m

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::d5e083c33faf98fd9cb61d287a35f2ff
https://doi.org/10.2514/6.2013-5169

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Decentralized Hybrid Flocking Guidance for a Swarm of Small UAVs

Autor: Heung-Sik Lim, Joonwon Choi, Hyunsam Myung, Yeongho Song, Seunghan Lim, Hyondong Oh

Publikováno v: Web of Science

Flocking is defined as flying in groups without colliding into each other through data exchange where each UAV applies a decentralized algorithm. In this paper, hybrid flocking control is proposed by using three types of guidance methods: vector fiel

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::4a55e82e74557b326b6cb171e31804ef
https://publons.com/wos-op/publon/54193543/

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