公开(公告)号：US3740004A

公开(公告)日：1973-06-19

申请号：US3740004D

申请日：1967-12-27

Applicant: BENDIX CORP

Inventor： DONIGER J ,  MORSE C ,  KNEMEYER S

IPC: G05D1/06 ,  B64C19/00

CPC classification number: G05D1/0607

Abstract: A system for guiding vertical flight of an aircraft to a predetermined aimpoint and including means for displaying for pilot information the angle between the line of sight of the craft to the predetermined aimpoint and the horizontal, the ground distance from the aircraft to the predetermined aimpoint, the ground speed of the aircraft, the time to reach the aimpoint and the angle between the aircraft velocity vector and the horizontal. The craft is guided during vertical maneuvers in response to a signal corresponding to the angle between the line of sight of the aircraft to the predetermined aimpoint and the horizontal, a signal corresponding to the angle between the aircraft velocity vector and the line of sight of the aircraft to the predetermined aimpoint, and a signal corresponding to the angle between the aircraft velocity vector and the horizontal.

Abstract translation: 一种用于将飞机的垂直飞行引导到预定瞄准点的系统，并且包括用于向飞行员信息显示飞行器的视线与预定瞄准点和水平面之间的角度，从飞行器到预定瞄准点的地面距离的装置， 飞机的地面速度，到达瞄准点的时间和飞机速度矢量与水平面之间的角度。 响应于对应于飞机的视线与预定瞄准点和水平线之间的角度的信号，在垂直操纵期间引导飞行器，对应于飞行器速度矢量与视线之间的角度的信号 飞机到预定目标点，以及对应于飞行器速度矢量和水平面之间的角度的信号。