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Applied flight dynamics modeling and stability analysis of a nonlinear time-periodic mono-wing aerial vehicle
FF Ahranjani, A Banazadeh - Aerospace Science and Technology, 2021 - Elsevier
This paper presents fly-ability, trim-ability, stability, and control ability of a mono-wing aerial
vehicle as an under-actuated multi-body system. A nonlinear mathematical model of this …
vehicle as an under-actuated multi-body system. A nonlinear mathematical model of this …
Feasibility study of attitude determination for all-rotating unmanned aerial vehicles in steady flight
All-rotating unmanned aerial vehicles (UAVs) are an interesting subgroup of unmanned
aerial vehicles because of their excellent aerodynamics and simple construction. The flight …
aerial vehicles because of their excellent aerodynamics and simple construction. The flight …
[HTML][HTML] 类 Samara 飞行器的曲线跟踪控制
练文钦， 孙洪飞 - Dynamical Systems and Control, 2022 - hanspub.org
Samara 飞行器是洛克希德· 马丁公司在枫树种子的启发下研发的一款单桨旋翼机,
它具有体积小, 重量轻, 气动效率高和隐蔽性**的特点. 但是Samara 飞行器的控制依赖于独立的 …
它具有体积小, 重量轻, 气动效率高和隐蔽性**的特点. 但是Samara 飞行器的控制依赖于独立的 …
[PDF][PDF] Razvoj elektronskega sistema za upravljanje vsevrtečega brezpilotnega letala
G Matič - 2015 - core.ac.uk
Pred nekaj leti se je znotraj skupine brezpilotnih letal z vrtečimi krili pojavila nova vrsta letal
z zanimivimi dinamičnimi in aerodinamičnimi lastnostmi, ki bi jo lahko poimenovali vsevrteča …
z zanimivimi dinamičnimi in aerodinamičnimi lastnostmi, ki bi jo lahko poimenovali vsevrteča …