PATENT CLAIM ANALYSIS

Application Number: 15752628
Application Type: Utility
Filing Date: 2018-02
Publication Date: 2019-01
Patent Classification: ["701", "100000"]

Abstract:
A control system for controlling a controlled parameter of an aeronautical equipment device, the controlled parameter being governed by an operating law linking the controlled parameter to a command and to a plurality of input parameters, the control system including a control loop controlling the controlled parameter to a setpoint with the control of the device by the command, the system including an operating law compensation module and a determination module determining a local gain configured to determine the local gain of a static part of a model of the operating law representative of the gain of the controlled parameter in response to a variation in the command in a stabilised operating regime of the operating law, the operating law compensation module using the inverse of the local gain.

Claim (Index 5):
The system of  claim 1 , wherein the determination module of the local gain is configured so that at least with each change of the command U and/or the input parameters, a new local gain is determined to reflect said changes.

Metadata:
- Claim Count in Document: 1.0
- Percentile: 88.0
- Lexical Diversity: 2.62745
- Patent Class: 701.0
- Transitional Phrase Type: none
- Component Type: 0
- Foreign Priority: True
- Related Applications: ['15526489', '12389812', '13885411', '10740340', '14906900']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.398076560927196
- 35 USC 102 Novelty (BERT): 0.5068513393224751
- Combined Prediction Score: 0.408954038766724
- Mean Citation Score: 169.96903999999995
- Max Citation Score: 197.82536
- Similarity Product: 115.73669842048167

Labels:
- Claim Label 101: 1
- Claim Label 102: 1
- Claim Label 103: 1
- Claim Label 112: 1
- Combined Label: 1
- Label 101 Adjusted: 0

Dataset: test