PATENT CLAIM ANALYSIS

Application Number: 15874709
Application Type: Utility
Filing Date: 2018-01
Publication Date: 2019-07
Patent Classification: ["701", "008000"]

Abstract:
A rotorcraft control system can include a controller configured to receive an input from a pilot or autopilot for controlling at least one of a rotor and/or a performance profile of the rotorcraft and to control a propulsor as a function of the input for controlling the propulsor relative to the rotor and/or for achieving the input performance profile, wherein the controller is configured to fly the aircraft in accordance with the performance profile or to conform manual control inputs to the performance profile.

Claim (Index 6):
The system of  claim 1 , wherein the input is a manual control input from at least one of a collective, a cyclic, a velocity, an attitude rate, an attitude, an acceleration, a thrust, and/or a throttle control.

Metadata:
- Claim Count in Document: 40.0
- Percentile: 86.0
- Lexical Diversity: 1.86957
- Patent Class: 701.0
- Transitional Phrase Type: none
- Component Type: 0
- Foreign Priority: False
- Related Applications: ['14741793', '14974988', '15248753', '11790971', '13908364']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.4879184675758605
- 35 USC 102 Novelty (BERT): 0.5104277327062363
- Combined Prediction Score: 0.4901693940888981
- Mean Citation Score: 252.73252
- Max Citation Score: 264.02695
- Similarity Product: 154.82975541652442

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

Dataset: test