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- W3022601102 abstract "Electrically driven mini drones are likely to have lower endurance than larger drones, mainly due to the limited aerodynamic efficiency of small, low elongation wings. The limited storage capacity of the on-board batteries on the mini-drones also reduces total endurance. The exploitation of aerodynamic interactions, inspired by migratory birds, as well as in-flight refuelling, are promising approaches to improve the endurance of mini-drones while allowing payload distribution.In the context of conventional aircraft formation flight, it was observed that a significant reduction in the following aircraft's energy consumption could be achieved by placing it in the wake vortices of the predecessor. In our context, this implies very precise displacements of the following mini-drone whose relative position (lateral and vertical) must remain at a fraction of the size of the predecessor mini-drone. In addition, the docking procedure used for exchanging batteries between UAVs in flight involves similar or even stricter guidance performance requirements. These strong performance constraints are also accompanied by particularly high robustness requirements on the control laws due to poorly known disturbances caused by wake turbulence.The work proposed in this thesis provides theoretical contributions aimed at enabling precise trajectory control thanks to advanced techniques based on a discrete-time predictive sliding-mode guidance scheme. On the other hand, we are also interested in advanced localization algorithms in order to feed collision avoidance strategies." @default.
- W3022601102 created "2020-05-13" @default.
- W3022601102 creator A5088333139 @default.
- W3022601102 date "2017-09-26" @default.
- W3022601102 modified "2023-09-23" @default.
- W3022601102 title "Contributions to Tight Formation Flight Control of Small UAS" @default.
- W3022601102 hasPublicationYear "2017" @default.
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