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 1):
A system for controlling a regulated parameter of an aeronautical equipment device, said regulated parameter being governed by an operating law of said aeronautical equipment device linking said regulated parameter to a command and to a plurality of input parameters, said operating law being modellable by a transfer function constituting a mathematical model of a relationship between the command, the input parameters, and the regulated parameter, said regulation control system comprising a regulation loop servo-controlling said regulated parameter at a setpoint through the command controlling the aeronautical equipment device,\n wherein the regulation loop comprises a regulator comprising in series a corrector and a compensation module of the operating law whereof a transfer function is intended to compensate the transfer function of the operating law, the command being delivered to the aeronautical equipment device corresponding to an output of the regulator, wherein the system further comprises a determination module of a local gain receiving the command and the input parameters, and configured to determine a local gain of a static part of a model of the operating law representative of a gain of said regulated parameter in response to a variation of said command in a steady operating state of said operating law, said static part of the model of the operating law combining time-independent relations between the regulated parameter, the command and the plurality of input parameters, said model of the operating law also comprising a dynamic part combining time-dependent relations between the regulated parameter, the command and the plurality of input parameters, said compensation module of the operating law involving an inverse of said local gain determined by the determination module.

Metadata:
- Claim Count in Document: 1.0
- Percentile: 88.0
- Lexical Diversity: 2.62745
- Patent Class: 701.0
- Transitional Phrase Type: open
- Component Type: 1
- Foreign Priority: True
- Related Applications: ['15526489', '12389812', '13885411', '10740340', '14906900']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.3737468300659191
- 35 USC 102 Novelty (BERT): 0.4884854344519184
- Combined Prediction Score: 0.385220690504519
- Mean Citation Score: 169.96903999999995
- Max Citation Score: 197.82536
- Similarity Product: 139.24279343729495

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

Dataset: test