Patent ID: 11878789
Assignee: AIRBUS OPERATIONS LIMITED
Field: Transport (Mechanical engineering)
Classification: CPC B | IPC B

Claim 1:
2. An aircraft brake control system as claimed in claim 1, wherein:
the second restriction level may be between 30 and 90% of the first restriction level; and/or
the mode controller is also configured to set a third mode, when the input of the indication of a brake energy supply configuration indicates a third brake energy supply being used, in which the antiskid brake calculator applies a third restriction level on a rise rate of the antiskid brake command, the third restriction level being lower than the second restriction level; and/or
a restriction level is variable, wherein optionally the control assembly comprises an input of an indication of a level of energy remaining in the brake energy supply and the restriction level is adjusted in dependence on the level of energy remaining; and/or
the antiskid brake calculator is configured to apply a specified minimum command level to the antiskid brake command.