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Minimum Fuel Circling Flight for Unmanned Aerial Vehicles in a Constant Wind

机译：恒定风速下无人机的最小燃油循环飞行

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The article of record as published may be located at http://arc.aiaa.org/doi/abs/10.2514/6.2008-6634

机译：已发布的记录文章可能位于http://arc.aiaa.org/doi/abs/10.2514/6.2008-6634

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Harada Masanori; Bollino Kevin;
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1. Minimum fuel powered dynamic soaring of unmanned aerial vehicles utilizing wind gradients [J] . Yiyuan J. Zhao, Ying Celia Qi Optimal Control Applications and Methods . 2004,第5期

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2. Verifiable Adaptive Flight Control: Unmanned Combat Aerial Vehicle and Aerial Refueling [J] . Jiang Wang∗ Naira Hovakimyan†Chengyu Cao‡ Journal of Guidance, Control, and Dynamics . 2010,第1期

机译：可验证的自适应飞行控制：无人驾驶飞机和空中加油
3. Verifiable Adaptive Flight Control: Unmanned Combat Aerial Vehicle and Aerial Refueling [J] . Jiang Wang, Naira Hovakimyan, Chengyu Cao Journal of guidance, control, and dynamics . 2010,第1期

机译：可验证的自适应飞行控制：无人驾驶飞机和空中加油
4. Minimum Fuel Circling Flight for Unmanned Aerial Vehicles in a Constant Wind [C] . M. Harada, K. Bollino AIAA guidance, navigation and control conference and exhibit . 2008

机译：恒定风速下无人机的最小燃油循环飞行
5. A flight time approximation model for unmanned aerial vehicles: Estimating the effects of flight dynamics and wind. [D] . Henchey, Matthew J. 2010

机译：无人机飞行时间近似模型：估算飞行动力学和风的影响。
6. Real-Time Model-Free Minimum-Seeking Autotuning Method for Unmanned Aerial Vehicle Controllers Based on Fibonacci-Search Algorithm [O] . Wojciech Giernacki, Dariusz Horla, Tomáš Báča, 2019

机译：基于斐波那契搜索算法的无人飞行器控制器实时无模型最小寻优自整定方法
7. Integrated Process Control‐Power Management System Design and Flight Performance Tests for Fuel Cell Powered Mini‐Unmanned Aerial Vehicle [O] . Betül Erdör Türk, Mustafa Hadi Sarul, Ekrem Çengelci, 2021

机译：集成过程控制 - 电源管理系统设计和飞行性能测试，用于燃料电池供电的迷你无人驾驶飞行器

Minimum Fuel Circling Flight for Unmanned Aerial Vehicles in a Constant Wind

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