Invention Grant
- Patent Title: Aircraft systems and methods for approach stabilization
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Application No.: US15791970Application Date: 2017-10-24
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Publication No.: US10600328B2Publication Date: 2020-03-24
- Inventor: Dorothee De Villele , Sharanabasappa Advani , Rajesh Chaubey
- Applicant: HONEYWELL INTERNATIONAL INC.
- Applicant Address: US NJ Morris Plains
- Assignee: HONEYWELL INTERNATIONAL INC.
- Current Assignee: HONEYWELL INTERNATIONAL INC.
- Current Assignee Address: US NJ Morris Plains
- Agency: Lorenz & Kopf, LLP
- Main IPC: G08G5/02
- IPC: G08G5/02 ; G05D1/06 ; B64D45/04 ; G08G5/00 ; G01C23/00

Abstract:
An enhanced flight management system and flight management method directed to improved guidance in unstable approach scenarios. The method includes receiving and processing a published arrival procedure (PAP), a published glide path (PGP), landing parameters, and real-time aircraft sensor data to determine a an actual approach profile, and whether the aircraft is following the reference approach profile. Approach stabilization criterion are determined, including, (i) a wind corrected air mass flight path angle (WC FPA) at the IMC; (ii) a vertical speed at the wind corrected air mass flight path angle (VS IMC); (iii) a wind corrected air mass flight path (WC FPA) angle at the VMC; and (iv) a vertical speed at the wind corrected air mass flight path angle (VS VMC). The method also determines whether an IMC criterion profile and a VMC criterion profile stabilizes the actual approach.
Public/Granted literature
- US20190122569A1 AIRCRAFT SYSTEMS AND METHODS FOR APPROACH STABILIZATION Public/Granted day:2019-04-25
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