aerodynamic control
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2021 ◽  
Vol 245 ◽  
pp. 112967
Author(s):  
Chaorong Zheng ◽  
Zhaoyong Wang ◽  
Jitong Zhang ◽  
Yue Wu ◽  
Zhao Jin ◽  
...  


2021 ◽  
Vol 1985 (1) ◽  
pp. 012040
Author(s):  
Wei Gao ◽  
Xinxin Kong ◽  
Zhaowen Deng ◽  
Wei Yu ◽  
Yongxing Wu ◽  
...  


2021 ◽  
Vol 212 ◽  
pp. 104600
Author(s):  
Z.X. Qiao ◽  
G. Minelli ◽  
B.R. Noack ◽  
S. Krajnović ◽  
V. Chernoray


2021 ◽  
Author(s):  
Benjamin Margolis ◽  
Wendy Okolo ◽  
Sarah N. D'Souza ◽  
Breanna J. Johnson




Author(s):  
S.G. Gendler ◽  
I.A. Borisovsky


2020 ◽  
Vol 117 (25) ◽  
pp. 254105
Author(s):  
Lawren Gamble ◽  
Aaron Lamoureux ◽  
Max Shtein
Keyword(s):  


Energies ◽  
2020 ◽  
Vol 13 (20) ◽  
pp. 5480
Author(s):  
Titilayo Ogunwa ◽  
Blake McIvor ◽  
Nurkhairunisa Awang Jumat ◽  
Ermira Abdullah ◽  
Javaan Chahl

The actuated abdomens of insects such as dragonflies have long been suggested to play a role in optimisation and control of flight. We have examined the effect of this type of actuation in the simplified case of a small fixed wing aircraft to determine whether energetic advantages exist in normal flight when compared to the cost of actuation using aerodynamic control surfaces. We explore the benefits the abdomen/tail might provide to balance level flight against trim changes. We also consider the transient advantage of using alternative longitudinal control effectors in a pull up flight maneuver. Results show that the articulated abdomen significantly reduces energy consumption and increase performance in isolated manoeuvres. The results also indicate a design feature that could be incorporated into small unmanned aircraft under particular circumstances. We aim to highlight behaviours that would increase flight efficiency to inform designers of micro aerial vehicles and to aid the analysis of insect flight behaviour and energetics.



2020 ◽  
Vol 2020 ◽  
pp. 1-12
Author(s):  
Guan Wang ◽  
Li Li ◽  
Weihua Li ◽  
Huajun Zhou ◽  
Changbo Ma ◽  
...  

This study investigates an adaptive controller for the flexible air-breathing hypersonic vehicles (AHVs) subject to external disturbances and actuator constraints. The combination of nonlinear disturbance observer and adaptive mechanism is exploited to design an adaptive controller for each subsystem. For the velocity subsystem, an auxiliary system is employed to handle the scramjet input saturation issue. For the altitude subsystem, the magnitude/rate constraints and the dynamics of aerodynamic control surfaces are addressed by the control allocation module. Simulations show the effectiveness of the proposed control.



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