Aircraft ground proximity warning system flight phase determination method based on data driving
A technology of flight phase and ground proximity warning, applied in the direction of neural learning methods, computer components, instruments, etc., can solve problems such as the inability to meet the diverse needs of aircraft types, different airframe states, and potential safety hazards, so as to improve identification accuracy, The effect of reducing data link dependence
- Summary
- Abstract
- Description
- Claims
- Application Information
AI Technical Summary
Problems solved by technology
Method used
Image
Examples
Embodiment 1
[0033] The present invention proposes a method of determining a method of time alarm system based on data-driven helicopter, the method comprising:
[0034] Gets the flight record data, performs data pretreatment of the flight record data, obtains the flight data sample P and the flight stage tag tag CK;
[0035] Generate a data set according to the flight data sample P and flight stage tag CK.
[0036] Construct neural network model;
[0037] Train the neural network model according to the flight data sample P and the flight stage tag Ck;
[0038] Get real-time flight data, enter the real-time flight data into the neural network model, and obtain the current flight stage of the helicopter through the neural network model.
[0039] Preferably, the flight recording data is acquired, and the flight recording data is pretreated, and the flight data sample P and the flight stage tag tag Ck are specifically include:
[0040] Through the corresponding channel of the helicopter, the coll...
Embodiment 2
[0059] Step 1: Get the flight recording data, perform data pretreatment of the flight record data, obtain the flight data sample P and the flight stage tag tag CK;
[0060] Specifically, according to the historical stored flight recording data, the preset time length t m The inner flight stage is an example, which will be described.
[0061] Step 1-1: The corresponding channel of the helicopter has a warning system, the collected flight full-stage cycle theme flight parameter data PD, recorded as [PD 1 ; PD 2 ; ...; PD tm ]
[0062] Among them, see Table 1, Pd 1 The vector combined with the aircraft in the aircraft, the current absolute air pressure height of the aircraft, the current absolute air pressure height, according to the preset time length t m PD inner 1 PD 2 , ..., PD tm , Get cycle theme flight parameter data PD matrix.
[0063] Table 1 cycle theme flight parameter data
[0064] serial number Flight parameters 1 Aircraft indicates air speed 2 Airpla...
PUM
Abstract
Description
Claims
Application Information
- R&D Engineer
- R&D Manager
- IP Professional
- Industry Leading Data Capabilities
- Powerful AI technology
- Patent DNA Extraction
Browse by: Latest US Patents, China's latest patents, Technical Efficacy Thesaurus, Application Domain, Technology Topic, Popular Technical Reports.
© 2024 PatSnap. All rights reserved.Legal|Privacy policy|Modern Slavery Act Transparency Statement|Sitemap|About US| Contact US: help@patsnap.com