公开(公告)号：US09117370B1

公开(公告)日：2015-08-25

申请号：US14205612

申请日：2014-03-12

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Matthew Pearson Jensen ,  Ivan Sandy Wyatt ,  Thea L. Feyereisen ,  Aaron Gannon

IPC: G06F19/00 ,  B64F1/20 ,  G01C21/00 ,  G08G5/06

CPC classification number: G08G5/065 ,  G08G5/0021 ,  G08G5/0065

Abstract: A system and method for determining if an aircraft is headed in the right direction on a runway entered upon at a location that does not display runway identification comprises receiving runway and aircraft position data for determining the identity of the runway. The identity of the runway is then compared with a representation of an assigned runway stored on the aircraft to determine that they match.

Abstract translation: 用于确定在不显示跑道识别的位置上输入的跑道上飞机是否朝向正确方向的系统和方法包括接收用于确定跑道身份的跑道和飞机位置数据。 然后将跑道的身份与存储在飞机上的指定跑道的表示进行比较，以确定它们匹配。

公开(公告)号：US20150081137A1

公开(公告)日：2015-03-19

申请号：US14028691

申请日：2013-09-17

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Aaron Gannon ,  Ivan Sandy Wyatt ,  Jary Engels ,  Steven P. Grothe

IPC: B64D45/00

CPC classification number: B64D45/00 ,  G01C23/005 ,  G08G5/0013 ,  G08G5/0021 ,  G10L15/26

Abstract: A system and method for validating data entry in response to an instruction received in an aircraft cockpit includes receiving, in an aircraft cockpit, an instruction that requires an aircraft pilot to manually enter a target value into an avionics system using an avionics system user interface. The received instruction is processed to determine the target value that should be set by the aircraft pilot using the avionics system user interface. Haptic feedback is to the avionics system user interface during the manual entry by the aircraft pilot.

Abstract translation: 用于响应于在飞行器驾驶舱中接收的指令来验证数据输入的系统和方法包括在飞行器驾驶舱中接收要求飞行员飞行员使用航空电子系统用户界面手动地将目标值输入到航空电子系统的指令。 处理接收到的指令以确定飞机飞行员应使用航空电子系统用户界面设置的目标值。 触觉反馈是航空器飞行员手动输入期间的航空电子系统用户界面。

公开(公告)号：US20140354456A1

公开(公告)日：2014-12-04

申请号：US13904241

申请日：2013-05-29

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Aaron Gannon ,  Ivan Sandy Wyatt ,  Troy Nichols ,  John G. Suddreth

IPC: G08G5/00

CPC classification number: G08G5/025 ,  G08G5/0021 ,  G08G5/0047

Abstract: A dynamic runway indicator is displayed overlying a conformal runway for assisting a pilot in completing an approach to landing on a runway. The dynamic runway indicator includes a polygon, that by changing position with respect to the conformal runway, provides advanced instrumentation cues to the pilot for adjusting the aircraft flight path to a normal, or recommended, path to the runway for landing, thereby assisting the pilot to improve the accuracy and safety of the approach and landing.

Abstract translation: 一个动态跑道指示器显示在一个保形跑道上，以协助飞行员完成在跑道上着陆的方法。 动态跑道指示器包括多边形，其通过相对于保形跑道改变位置，向飞行员提供高级仪表线索，用于调整飞行器飞行路径到达跑道的正常或推荐路径以降落，从而辅助飞行员 提高进场和落地的准确性和安全性。

公开(公告)号：US20140288733A1

公开(公告)日：2014-09-25

申请号：US13847151

申请日：2013-03-19

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Gang He ,  Ivan Sandy Wyatt

IPC: G08G5/02 ,  G01C21/00

CPC classification number: G08G5/02 ,  G01C21/005 ,  G01S19/15 ,  G01S19/23 ,  G01S19/47 ,  G08G5/025

Abstract: Systems and methods for reducing error detection latency in LPV approaches are provided. In certain embodiments, a method for navigational guidance includes calibrating inertial measurements acquired from an inertial navigation system with satellite-based augmentation system position measurements acquired from a satellite-based augmentation system to create corrected inertial navigation system positions. The method also includes determining whether the satellite-based augmentation system experienced a fault when the inertial measurements were calibrated with the satellite-based augmentation system position measurements. Further, when the satellite-based augmentation system did not experience a fault, the method includes monitoring the satellite-based augmentation system navigation position measurements based on the corrected inertial navigation system positions.

Abstract translation: 提供了用于减少LPV方法中的错误检测延迟的系统和方法。 在某些实施例中，用于导航指导的方法包括校准从惯性导航系统获得的惯性测量，其具有从基于卫星的增强系统获取的基于卫星的增强系统位置测量值，以创建校正的惯性导航系统位置。 该方法还包括当使用基于卫星的增强系统位置测量校准惯性测量时，确定基于卫星的增强系统是否经历故障。 此外，当基于卫星的增强系统没有遇到故障时，该方法包括基于校正的惯性导航系统位置监视基于卫星的增强系统导航位置测量。

公开(公告)号：US20140222257A1

公开(公告)日：2014-08-07

申请号：US13759408

申请日：2013-02-05

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Ivan Sandy Wyatt ,  Gang He ,  Thea L. Feyereisen

IPC: B64D45/08

CPC classification number: B64D45/08 ,  G08G5/0021 ,  G08G5/02 ,  G08G5/025

Abstract: A system and method is disclosed for anticipating a missed approach point (MAP) during an instrument landing of an aircraft. Symbology is generated and displayed that graphically represents a lateral distance between a runway threshold and a virtual inner marker. The MAP is identified as the location of the aircraft when the symbology reaches a displayed runway threshold.

Abstract translation: 公开了一种用于在飞机的仪表着陆期间预期错过的接近点（MAP）的系统和方法。 生成和显示符号学，其以图形方式表示跑道阈值和虚拟内标记之间的横向距离。 当符号系统达到显示的跑道阈值时，MAP被标识为飞机的位置。