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公开(公告)号:US09604719B2
公开(公告)日:2017-03-28
申请号:US14167095
申请日:2014-01-29
Applicant: AIRBUS OPERATIONS S.A.S.
Inventor: Matthieu Mayolle , Caroline Acanfora , Louis-Emmanuel Romana , Julien Fontan
CPC classification number: B64C25/48 , B60T8/1703 , B60T2201/16 , B64C25/50
Abstract: A device for lateral control of an aircraft includes a calculating unit for automatically applying, if conditions for turning of the aircraft are met, a symmetrical braking value at a brake assembly. Subsequently, in the course of the turn, the device automatically distributes this symmetrical braking value in differential braking between a braking device of the left main landing gear and a braking device of the right main landing gear of the aircraft. Distribution of the symmetrical breaking is performed as a function of current directional command orders in such a way as to maintain a constant overall braking level for, at least for directional command orders below a predetermined threshold.
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公开(公告)号:US11816024B2
公开(公告)日:2023-11-14
申请号:US17586913
申请日:2022-01-28
Applicant: AIRBUS OPERATIONS LIMITED , AIRBUS OPERATIONS (S.A.S.)
Inventor: Louis-Emmanuel Romana , George Howell
IPC: G06F11/36
CPC classification number: G06F11/3692 , G06F11/3684 , G06F11/3688
Abstract: A method of testing a system model is disclosed. The system model includes a system parameter and three or more equipment models, each equipment model includes an equipment parameter which models a parameter of a respective equipment. The method includes (a) making a series of changes of the equipment parameter of one of the equipment models so that the equipment parameter of the one of the equipment models adopts a series of test values of the equipment parameter; (b) operating the system model to determine a series of test values of the system parameter, each test value of the system parameter is determined in accordance with a respective one of the test values of the equipment parameter; (c) determining a weight of the selected one of the equipment models, the weight of the one of the equipment models indicates a sensitivity of the system parameter to the series of changes in the equipment parameter of the one of the equipment models; and (d) outputting the weight of the one of the equipment models.
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