Integrated thrust reverser and brake control for an aircraft

A method comprising:

• detecting, by a control system of an aircraft, a landing condition of the aircraft;
• determining, by the control system, one or more thrust reverser deployment and brake control parameters for one or more current conditions at a target location of the aircraft;
• controlling, by the control system, the one or more thrust reversers and the one or more brakes upon landing at the target location based on the one or more thrust reverser deployment and brake control parameters;
• and
• modifying, by the control system, one or more control parameters of the aircraft based on detecting a change in the one or more current conditions at the target location or a fault condition of the aircraft.

A method comprising:

• detecting, by a control system of an aircraft, a takeoff mode of the aircraft;
• monitoring, by the control system, for one or more failure conditions of the aircraft;
• controlling, by the control system, one or more thrust reversers and one or more brakes of the aircraft based on detecting that the one or more failure conditions should result in a rejected takeoff;
• and
• modifying, by the control system, one or more control parameters of the aircraft based on detecting a thrust reverser fault and/or a brake fault during the rejected takeoff.