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 9):
The system of  claim 8 , wherein the controller is configured to output a performance profile deviation or disengage signal to an indicator in the event of unplanned acceleration and/or other unplanned motion outside of the performance profile due to one or more smart autopilot routines and/or due to manual unplanned control of the aircraft.

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): 0.4894744858708619
- 35 USC 102 Novelty (BERT): 0.5029203002461922
- Combined Prediction Score: 0.490819067308395
- Mean Citation Score: 252.73252
- Max Citation Score: 264.02695
- Similarity Product: 178.4834139778793

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

Dataset: test