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公开(公告)号:US20240166384A1
公开(公告)日:2024-05-23
申请号:US18388171
申请日:2023-11-08
Applicant: THALES
Inventor: Marc RIEDINGER , Eric GUILLOUET , Antoine BONNET , Patrick GOUHIER
IPC: B64U20/87 , B64U20/70 , B64U50/20 , G01S13/933
CPC classification number: B64U20/87 , B64U20/70 , B64U50/20 , G01S13/933
Abstract: An unmanned aircraft includes three parallel beams extending in at least one longitudinal direction X from a rear side to a front side of the aircraft, the central beam forming a main fuselage containing a powertrain, with a propeller of diameter D configured to be driven by the powertrain being attached to a front end of the central beam, each side beam being at a distance L/2 from the central beam and each side beam supporting a radar at a front end of the beam.
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公开(公告)号:US20230205204A1
公开(公告)日:2023-06-29
申请号:US17923488
申请日:2021-05-03
Applicant: THALES
Inventor: Laurent LALUQUE , Sylvain LISSAJOUX , Patrick GOUHIER , Bruno CAPELLE
CPC classification number: G05D1/0055 , G05D1/0088 , B64U10/00 , B64U2201/10
Abstract: Method for controlling an unmanned aircraft piloted by a fully autonomous control system including a first decision module and a simplex piloting control module including a high-performance controller, a high-safety controller and a second decision module, the high-performance and high-safety controllers determining piloting commands for the robot-aircraft, according to which: —as long as a set of conditions is verified, implementation by the first decision module of a nominal piloting mode with delivery to the output of the automatic control system of the piloting commands delivered to the output of the simplex piloting control module; —otherwise, switching to an emergency piloting mode, an emergency piloting command is delivered to the output of the automatic control system for execution by the robot-aircraft, the first decision module preventing the delivery to the output of the automatic control system of the piloting commands delivered to the output of the simplex module.
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