Verifying the effect of wingtip propellers on drag through in-flight measurements
This work presents the effect of wingtip-mounted propellers on the aircraft drag polar,
identified from in-flight measurements. In previous wind-tunnel experiments, significant …
identified from in-flight measurements. In previous wind-tunnel experiments, significant …
Flight dynamics and control assessment for differential thrust aircraft in engine inoperative conditions including aero-propulsive effects
MFM Hoogreef, JSE Soikkeli - CEAS Aeronautical Journal, 2022 - Springer
Differential thrust can be used for directional control on distributed electric propulsion
aircraft. This paper presents an assessment of flight dynamics and control under engine …
aircraft. This paper presents an assessment of flight dynamics and control under engine …
Consensus-Based Powered Cruise and Yaw Controls for Unmanned Aerial Vehicle with Distributed Electric Propulsion System
The distributed electric propulsion (DEP) system has been favored over the conventional
centralized propulsion system in applications of unmanned aerial vehicles (UAV). However …
centralized propulsion system in applications of unmanned aerial vehicles (UAV). However …
Integration of propelled yaw control on wing tips: a practical approach to the Icaré solar-powered glider
J Schneider, M Frangenberg, S Notter… - CEAS Aeronautical …, 2022 - Springer
In this practical approach to distributed propulsion, the solar-powered manned motorglider
icaré 2 has been used as a testbed for wingtip propulsion. The large wingspan and slow …
icaré 2 has been used as a testbed for wingtip propulsion. The large wingspan and slow …
Incremental Control Allocation with Axis Prioritization on the Boundary of the Attainable Control Set
View Video Presentation: https://doi. org/10.2514/6.2023-1639. vid Pseudoinverse-based
control allocation provides a computationally efficient way of allocating desired pseudo …
control allocation provides a computationally efficient way of allocating desired pseudo …
[PDF][PDF] 分布式电推进飞机动力偏航非线性动态逆控制
尤顺， 寇鹏， 姚轩宇， 王京， 梁得亮， 梁哲 - Journal of Aerospace Power, 2024 - jasp.com.cn
分布式电推进飞机可通过多推进器间的推力差动来调节飞行姿态, 从而为实现动力偏航提供了
硬件条件. 为此, 提出一种基于非线性动态逆的动力偏航控制策略. 建立考虑分布式电推进系统 …
硬件条件. 为此, 提出一种基于非线性动态逆的动力偏航控制策略. 建立考虑分布式电推进系统 …
Multivariable Fault Tolerant Control for a Distributed Electric Propulsion Aircraft
G Morani, L Garbarino, N Genito… - AIAA SCITECH 2024 …, 2024 - arc.aiaa.org
This paper describes a control strategy for an aircraft with distributed electric propulsion and
conventional aerodynamic control surfaces. Control algorithms are made of multivariable …
conventional aerodynamic control surfaces. Control algorithms are made of multivariable …
Nonlinear dynamic inversion for the powered yaw control of distributed electric propulsion aircraft
YOU Shun, KOU Peng, YAO Xuanyu, W Jing, L Deliang… - 航空动力学报, 2024 - jasp.com.cn
Distributed electric propulsion aircraft makes it possible for additional control authority by
differential thrust, thus giving rise to the concept of powered yaw control. A powered yaw …
differential thrust, thus giving rise to the concept of powered yaw control. A powered yaw …
Cascaded nonlinear dynamic inversion applied to a fixed-wing distributed electric propulsion aircraft
JS Soikkeli, D Matko, T Koopman - AIAA AVIATION 2023 Forum, 2023 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2023-4048. vid This paper presents a
cascaded nonlinear dynamic inversion flight control design for a fixed-wing distributed …
cascaded nonlinear dynamic inversion flight control design for a fixed-wing distributed …