The invention discloses an aircraft landing brake distance control method. The method comprises the steps of acquiring a deceleration path of an aircraft on a runway, a deceleration distance of the deceleration path, an end point speed at an end point of the deceleration path and a running speed at a starting point of the deceleration path; calculating a deceleration rate according to the deceleration distance, the running speed and the end point speed; and controlling the aircraft to decelerate on the runway according to the deceleration rate. The deceleration distance of the aircraft runway and the end point speed of the deceleration distance end point are obtained firstly, then the running speed of the aircraft initial position is obtained, and the deceleration rate can be obtained according to the deceleration distance, the end point speed and the running speed; and the aircraft can be controlled to decelerate according to the deceleration rate, and the aircraft can be decelerated to the end speed at the end position of the deceleration distance in the runway.
发明公开了一种飞行器着陆刹车距离控制方法,包括:获取飞行器在跑道上的减速路径、减速路径的减速距离、减速路径终点处的终点速度和减速路径起点处的行驶速度;根据减速距离、行驶速度、终点速度计算减速率;根据减速率控制飞行器在跑道上减速。本公开通过首先获取飞行器跑道的减速距离和减速距离终点的终点速度然后获取飞行器初始位置的行驶速度,根据减速距离、终点速度和行驶速度,可以获得减速率;可以根据该减速率来控制器飞行器减速,可以在跑道中减速距离的终点位置完成减速至终点速度。
Aircraft landing brake distance control method
一种飞行器着陆刹车距离控制方法
2021-06-01
Patent
Electronic Resource
Chinese
IPC: | B60T Bremsanlagen für Fahrzeuge oder Teile davon , VEHICLE BRAKE CONTROL SYSTEMS OR PARTS THEREOF |
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