Invention Grant
- Patent Title: Systems and methods for providing throttle guidance as a function of flight path acceleration
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Application No.: US16672105Application Date: 2019-11-01
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Publication No.: US11299285B2Publication Date: 2022-04-12
- Inventor: Luis Melendez , Philip Sin , John Koenig
- 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: B64D31/06
- IPC: B64D31/06 ; B64F5/60

Abstract:
Technologically improved vehicle control systems and methods are described. The provided vehicle control systems and methods embody an inner loop auto-throttle control for causing delta-throttle changes, i.e., servo changes, to achieve desired acceleration targets. The system generates an error on a potential flight path angle using a received thrust acceleration command. The error on the potential flight path angle is converted into an equivalent acceleration. A throttle rate command TLA_ratecmd is generated by converting the equivalent acceleration into the throttle rate command TLA_ratecmd.
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