System for controlling an aircraft thrust reversal means

A method for controlling a thrust reverser system connected to at least one engine of an aircraft, wherein the thrust reverser system comprises a detector, a speed detector, a radio altimeter, a position sensor, and levers comprising:

• detecting a condition for activation of a reverse idle control by:
• collecting speed detected by the speed detector,
• collecting an altitude emitted by the radio altimeter,
• determining a position of the levers, and
• determining the angle of descent or climb of the aircraft,
• activating the reverse idle control,
• detecting a condition for activation of the thrust reverser by:
• determining if the weight of the aircraft rests on wheels of landing gear;
• and
• when the weight of the aircraft rests on the wheels of the landing gear, activating the thrust reverser, and
• detecting a condition for activation of the reverse idle control.