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Contents

Navigation Augmentation in Urban Area by HALE UAV with Onboard Pseudolite during Multi-Purpose Missions / O-Jong Kim ; Sunkyoung Yu ; Heekwon No ; Changdon Kee ; Minwoo Choi ; Hyojeong Seok ; Donghwan Yoon ; Byungwoon Park ; Cheolkyu Jee 1

Abstract 1

1. Introduction 1

2. HALE UAV 3

2.1. HALE UAV Configuration 3

2.2. Altitude Cycle of HALE UAV 3

2.3. Velocity of HALE UAV 3

2.4. Pseudolite in HALE UAV 3

3. Simulation Environments 4

3.1. Simulation Area 4

3.2. Wind Speed over Korea 4

3.3. GPS and HALE UAV Trajectories for Simulations 5

3.4. Flight Scenarios 5

4. Simulation Results 6

4.1. Simulation Results of Teheran Street 6

4.2. Simulation Results in Posco-intersection 8

5. Conclusion 9

References 9

권호기사

권호기사 목록 테이블로 기사명, 저자명, 페이지, 원문, 기사목차 순으로 되어있습니다.
기사명 저자명 페이지 원문 목차
Operation Limit of Flow Control for a Bistable Fluidic Valve Ji Ung Lee, Ji-Seok Hong, Hong-Gye Sung pp.389-394

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Heat Transfer and Frictions in the Convergent/divergent Channel with Λ/V-shaped Ribs on Two Walls Beom-soo Kim, Myung-sung Lee, Soo-whan Ahn pp.395-402

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Multi-Point Aerodynamic Design Optimization of DLR F-6 Wing-Body-Nacelle-Pylon Configuration Takashi Saitoh, Hyoungjin Kim, Keizo Takenaka, Kazuhiro Nakahashi pp.403-413

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MSBS-SPR Integrated System Allowing Wider Controllable Range for Effective Wind Tunnel Test Yeol-Hun Sung, Dong-Kyu Lee, Jong-Seob Han, Ho-Young Kim, Jae-Hung Han pp.414-424

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Overview of Flow Diagnosis in a Shock Tunnel Ikhyun Kim, Sungmin Lee, Gisu Park, Jong Kook Lee pp.425-435

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Multi-scale Progressive Failure Analysis of Triaxially Braided Textile Composites Tsinuel N. Geleta, Kyeongsik Woo pp.436-449

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An Approximate Method for the Buckling Analysis of a Composite Lattice Rectangular Plate Yongha Kim, Pyunghwa Kim, Hiyeop Kim, Jungsun Park pp.450-466

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Effect of Three-dimensional Warping on Stiffness Constants of Closed Section Composite Beams Manoj Kumar Dhadwal, Sung Nam Jung pp.467-473

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Application of Artificial Neural Networks to Predict Dynamic Responses of Wing Structures due to Atmospheric Turbulence Anh Tuan Nguyen, Jae-Hung Han, Anh Tu Nguyen pp.474-484

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Structural Dynamic Analysis of a Space Launch Vehicle using an Axisymmetric Two-dimensional Shell Element JiSoo Sim, SangGu Lee, JunBeom Kim, SangJoon Shin, SeungSoo Park, WonSuk Ohm pp.485-497

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Validation of Loads Analysis for a Slowed Rotor at High Advance Ratios Jae-Sang Park pp.498-511

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Development of a University-Based Simplified H₂O₂/PE Hybrid SoundingRocket at KAIST Jeongmoo Huh, Byeonguk Ahn, Youngil Kim, Hyunki Song, Hosung Yoon, Sejin Kwon pp.512-521

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Consensus of Leader-Follower Multi-Vehicle System Enjiao Zhao, Tao Chao, Songyan Wang, Ming Yang pp.522-534

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An Improved Hybrid Kalman Filter Design for Aircraft Engine based on a Velocity-Based LPV Framework Xiaofeng Liu pp.535-544

보기
Navigation Augmentation in Urban Area by HALE UAV with Onboard Pseudolite during Multi-Purpose Missions O-Jong Kim, Sunkyoung Yu, Heekwon No, Changdon Kee, Minwoo Choi, Hyojeong Seok, Donghwan Yoon, Byungwoon Park, Cheolkyu Jee pp.545-554

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Vibration-Robust Attitude and Heading Reference System Using Windowed Measurement Error Covariance Jong-Myeong Kim, Sung-Hoon Mok, Henzeh Leeghim, Chang-Yull Lee pp.555-564

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A Multistage In-flight Alignment with No Initial Attitude References for Strapdown Inertial Navigation Systems WoonSeon Hong, Chan Gook Park pp.565-573

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Distributed and Real-time Integrated Simulation System on Avionics Yaoming Zhou, Yaolong Liu, Shaowei Li, Yuhong Jia pp.574-578

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Numerical Feasibility Study for a Spaceborne Cooler Dual-function Energy Harvesting System Seong-Cheol Kwon, Hyun-Ung Oh pp.579-587

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Automated Wireless Recharging for Small UAVs Sunghun Jung, Kartik B. Ariyur pp.588-600

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참고문헌 (21건) : 자료제공( 네이버학술정보 )

참고문헌 목록에 대한 테이블로 번호, 참고문헌, 국회도서관 소장유무로 구성되어 있습니다.
번호 참고문헌 국회도서관 소장유무
1 “NASA Armstrong Fact Sheet: Helios Prototype [Internet]”, 2014 [cited 2014 Feb 28], Available from: http:// www.nasa.gov/centers/dryden/news/FactSheets/FS-068- DFRC.html 미소장
2 “QinetiQ's Zephyr Solar Aircraft Double Award by IET [Internet]”, 2011 [cited 2011 Nov 10], Available from: http:// www.qinetiq.com/media/news/releases/Pages/Zephyrwins- two-awards.aspx 미소장
3 “Another First for Airbus Zephyr 7: Successful SatCom- Controlled High Altitude Pseudo-Satellite Test Flight in Winter Weather Conditions [Internet]”, 2014 [cited 2014 Aug 29], Available from: http://airbusdefenceandspace.com/another-first-for-airbus-zephyr-7/ 미소장
4 “About Global Observer: Maximum Endurance, Maximum Coverage, Affordable cost (Official Webpage) [Internet]”, 2015, Available from: https://www.avinc.com/globalobserver/about/ 미소장
5 “Phantom Eye (Official Webpage) [Internet]”, 2015, Available from: http://www.boeing.com/boeing/bds/ phantom_works/phantom_eye.page 미소장
6 “Global Hawk (Official Webpage) [Internet]”, 2015, Available from: http://www.northropgrumman.com/ Capabilities/GlobalHawk/Pages/default.aspx 미소장
7 Development of Korean High Altitude Platform Systems 네이버 미소장
8 Wing Design Optimization of a Solar-HALE Aircraft 소장
9 Computational Analysis of the Aerodynamic Performance of a Long-Endurance UAV 소장
10 Pseudolites 네이버 미소장
11 Cobb, H. S., GPS Pseudolites: Theory, Design, and Applications, Ph.D. Dissertation, Stanford University, Stanford, CA, USA, Sep. 1997. 미소장
12 Increasing the Spatial Limits of LADGPS Using Stratospheric Platforms 네이버 미소장
13 Dovis, F., Mulassano, P. and Dumville, M., “The Stratolite Concept: Design of a Stratospheric Pseudo- Satellite for Galileo”, Proceedings of ION GPS 2002, Portland, OR, USA, 2002. 미소장
14 Tsujii, T., Harigae, M. andOkano, K., “A New Positioning/Navigation System Based on Pseudolites Installed on High Altitude Platforms Systems (HAPS)”, Proceedings of 24th International Congress of the Aeronautical Sciences, Yokohama, Japan, 2004. 미소장
15 Tsujii, T., Harigae, M., Barnes, J., Wang, J. and Rizos, C., “Experiments of Inverted Pseudolite Positioning for Airship- Based GPS Augmentation System”, Proceedings of ION GPS 2002, Portland, OR, 2002. 미소장
16 Sklar, J. R., “Interference Mitigation Approaches for the Global Positioning System”, Lincoln Laboratory Journal, Vol. 14, No. 2, 2003, pp. 167-180. 미소장
17 Kim, O., Choi, M., Yu, S., No, H., Seok, H., Yoon, D., Park, B., Kee, C. and Jee, C., “Navigation Augmentation in Urban Area with Pseudolite Equipped High Altitude Long Endurance UAV”, Proceedings of 2015 International Technical Meeting of ION, Dana Point, CA, 2015. 미소장
18 Shin, K., Hwang, H. and Ahn, J., “Initial Climb Mission Analysis of a Solar HALE UAV”, Journal of the Korean Society for Aeronautical and Space Sciences (Korean Language), Vol. 42, No. 4, 2014, pp. 468-477. DOI:10.5139/ JKSAS.2014.42.6.468 미소장
19 Park, K., Min, S., Ahn, J. and Lee, D., “Multidisciplinary Design Optimization (MDO) of a Medium-Sized Solar Powered HALE UAV Considering Energy Balancing”, Journal of the Korean Society for Aeronautical and Space Sciences (Korean Language), Vol. 40, No. 2, 2012, pp. 129-138. DOI:10.5139/JKSAS.2012.40.2.129 미소장
20 Whitfield, C. A., An Adaptive Dual-Optimal Path- Planning Technique for Unmanned Air Vehicles with Application to Solar-Regenerative High Altitude Long Endurance Flight, Ph.D. Dissertation, The Ohio State University, 2009. 미소장
21 Overview of GPS Operation and Design 네이버 미소장

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