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Nonlinear Dynamical Modeling of a High Altitude Long Endurance Unmanned Aerial Vehicle

机译：高空长寿命无人机的非线性动力学建模

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《AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference》|2009年|P.1-11|共11页
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I. Tuzcu; P. Marzocca; K. Awni;
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原文格式 PDF
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中图分类航空;
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4. Nonlinear Dynamical Modeling of a High Altitude Long Endurance Unmanned Aerial Vehicle [C] . American Institute of Aeronautics and Astronautics/American Society of Mechanical Engineers/American Society of Civil Engineers/Vertical Flight Technical Society/ASC Structures, Structural Dynamics, and Materials Conference . 2009

机译：高海拔长耐力无人空中车辆的非线性动力学建模
5. Optimal Lateral Guidance for Automatic Landing of a Lightweight High Altitude Long Endurance Unmanned Aerial System with Crosswind Rejection. [D] . Smith, Nathan Allen. 2016

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7. The impact of altitude, latitude, and endurance duration on the design of a high altitude, solar powered unmanned aerial vehicle [O] . Ahmad Alsahlani, Thurai Rahulan 2016

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8. Innovative Management in the DARPA High Altitude Endurance Unmanned Aerial Vehicle Program. Phase 2 Experience [R] . Drezner, J. A. , Sommer, G. , Leonard, R. S. 1999

机译：DaRpa高海拔耐力无人机项目的创新管理。第二阶段经验

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