Non-binary collaborative recovery system

A technology of recovery system and flight control system, applied in the field of aircraft flight envelope protection system, which can solve the problem of not being suitable for commercial or commercial aircraft, etc.

Pending Publication Date: 2021-04-09
GULFSTREAM AEROSPACE CORP
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

This might work for a military aircraft, with the pilot wearing a helmet, strapped into the ejection seat system, ready to absorb the hard recovery g-forces, but not for a commercial or commercial aircraft

Method used

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  • Non-binary collaborative recovery system
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Embodiment Construction

[0023] The following detailed description is merely exemplary in nature and is not intended to limit the invention or the application and uses of the invention. Furthermore, there is no intention to be bound by any theory presented in the preceding background section or the following detailed description.

[0024] introduction

[0025] The disclosed aircraft flight envelope protection system uses flight path prediction techniques to provide a unified full envelope protection that operates over a full range of aircraft flight conditions for a full range of different types of hazards. A flight path prediction is continuously calculated from the current condition of the aircraft using a kinetic energy model. A plurality of predicted trajectories are computed, each representing a different escape route that enables recovery from the hazard when the hazard's threshold or trigger point is reached. The system considers different types of hazards, some involving inherent properties ...

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Abstract

A processor supplies flight commands to the flight control system by selectively blending pilot input with control signals from the autopilot. The processor generates a projected recovery trajectory through successive iterations, each beginning at the current aircraft location and using a recovery constraint selectable by the processor to influences a degree of flight aggressiveness. A detection system that identifies and invokes a state of threat existence if a threat exists along the projected recovery trajectory. The processor during threat existence in a first iteration commands an initial soft recovery, with permitted blended pilot input. If the threat exists on subsequent iteration, the processor commands a more aggressive recovery while attenuating blended pilot input.

Description

[0001] priority claim [0002] Pursuant to 35 U.S.C. §229(e), this application claims priority to U.S. Provisional Application No. 62 / 723,187, filed August 27, 2018, entitled "AircraftFlight Envelope Protection Framework," the entire disclosure, drawings, and appendices Included herein by reference. technical field [0003] The present disclosure relates generally to aircraft flight envelope protection systems, and more particularly to aircraft flight envelope protection systems that model potential aircraft trajectories and test those trajectories for aircraft restriction violations and terrain avoidance hazards. Background technique [0004] This section provides background information related to the present disclosure which is not necessarily prior art. [0005] Aircraft are designed to operate within certain operating speeds and loads with respect to the control surfaces of the aircraft. These operating limits are known as the flight envelope, outside of which it is po...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05D1/10
CPCG05D1/106G08G5/0086G08G5/0021G08G5/045G05D1/1064G08G5/0078G08G5/0091G05D1/0061G05D1/0088G05D1/0816G08G5/0039G08G5/006G08G5/04G06F18/251
Inventor 凯文·普洛瑟T·兰德斯A·萨哈伊A·维迪亚B·芬莱森
Owner GULFSTREAM AEROSPACE CORP
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