公开(公告)号：EP0438816B1

公开(公告)日：1995-09-06

申请号：EP90202722.6

申请日：1990-10-11

申请人： THE BOEING COMPANY

发明人： Orgun, Munir ,  McRoberts, Timothy Clark ,  Virdee, Arvinder Sing

IPC分类号： G05D1/00 ,  B64D31/10 ,  G05D1/08

CPC分类号： G05D1/0676 ,  G05D1/0072

公开(公告)号：EP0438816A1

公开(公告)日：1991-07-31

申请号：EP90202722.6

申请日：1990-10-11

申请人： THE BOEING COMPANY

发明人： Orgun, Munir ,  McRoberts, Timothy Clark ,  Virdee, Arvinder Sing

IPC分类号： G05D1/00 ,  B64D31/10 ,  G05D1/08

CPC分类号： G05D1/0676 ,  G05D1/0072

摘要： Disclosed is a method of and apparatus for processing flight control signals in an automatic landing system so that automatic landings can be executed within the bounds of current certification requirements (Category III weather minimums) and in a manner that in effect emulates standard manual landing procedures. Included is provision for introducing engine-out sideslip that insures that the automatic landing approach and touchdown is made with the aircraft wings level or with the upwind wing low. Also provided is the generation of rudder and wheel (aileron) compensation for lateral ground effects that occur during a landing with sideslip when the aircraft altitude is approximately one wingspan or less. Provision also is made for rudder control to offset yawing moment that occurs when the thrust of the operative engines is retarded prior to touchdown. A two stage alignment procedure is provided for use in both engine-out automatic landings and normal automatic landings to decrab the aircraft throughout a moderately light to relatively high crosswind range.

摘要翻译： 公开了一种用于在自动着陆系统中处理飞行控制信号的方法和装置，使得可以在当前认证要求（III类天气最小值）的范围内执行自动着陆并且以实际上模拟标准手动登陆程序的方式执行自动着陆。 包括引入发动机侧滑的条款，确保自动着陆方式和达阵与飞机机翼水平或上风翼低。 还提供了当飞机高度大约为一个翼展或更小时，在侧滑时着陆时发生的侧向地面效应的舵和轮（副翼）补偿的产生。 还提供了方向舵控制以抵消在触地之前延迟操作发动机的推力时发生的偏航力矩。 提供两级对准程序，用于发动机自动着陆和正常自动着陆，以在适度轻到相对较高的侧风范围内解除飞行器。