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公开(公告)号:US20230017711A1
公开(公告)日:2023-01-19
申请号:US17784930
申请日:2020-12-14
发明人: Kevin Garanger , Jeremy Epps , Eric Feron , Michael Miller
摘要: A fractal unmanned aircraft system (200) includes a first module (100), a second module (100) and a third module, (100) each having a top member (120) and a first thruster (130) affixed thereto. Each module (100) is laterally coupled to each other. A fourth module (100) has a bottom that is affixed to the top members (120) of the first module(100), the second module (100) and the third module (100) so as to form a tetrahedral structure. A power source (220) supplies power to the first thrusters (130). A control circuit (222) controls the unmanned aircraft system so as to cause the fractal unmanned aircraft system (200) to fly in a controlled manner.
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公开(公告)号:US11970268B2
公开(公告)日:2024-04-30
申请号:US17784930
申请日:2020-12-14
发明人: Kevin Garanger , Jeremy Epps , Eric Feron , Michael Miller
CPC分类号: B64C39/024 , B64C25/32 , B64C37/02 , B64D27/24 , B64U30/20 , B64U50/19 , B64U2201/20
摘要: A fractal unmanned aircraft system (200) includes a first module (100), a second module (100) and a third module, (100) each having a top member (120) and a first thruster (130) affixed thereto. Each module (100) is laterally coupled to each other. A fourth module (100) has a bottom that is affixed to the top members (120) of the first module (100), the second module (100) and the third module (100) so as to form a tetrahedral structure. A power source (220) supplies power to the first thrusters (130). A control circuit (222) controls the unmanned aircraft system so as to cause the fractal unmanned aircraft system (200) to fly in a controlled manner.
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