PATENT CLAIM ANALYSIS

Application Number: 16271916
Application Type: Utility
Filing Date: 2019-02
Publication Date: 2019-10
Patent Classification: ["701", "002000"]

Abstract:
An aircraft defining an upright orientation and an inverted orientation, a ground station; and a control system for remotely controlling the flight of the aircraft. The ground station has an auto-land function that causes the aircraft to invert, stall, and controllably land in the inverted orientation to protect a payload and a rudder extending down from the aircraft. In the upright orientation, the ground station depicts the view from a first aircraft camera. When switching to the inverted orientation: (1) the ground station depicts the view from a second aircraft camera, (2) the aircraft switches the colors of red and green wing lights, extends the ailerons to act as inverted flaps, and (3) the control system adapts a ground station controller for the inverted orientation. The aircraft landing gear is an expanded polypropylene pad located above the wing when the aircraft is in the upright orientation.

Claim (Index 4):
The method of  claim 1 , wherein the one or more control surfaces include one or more elevators on an empennage, and wherein step (c) includes controlling the operation of the one or more elevators.

Metadata:
- Claim Count in Document: 4.0
- Percentile: 99.0
- Lexical Diversity: 2.18421
- Patent Class: 701.0
- Transitional Phrase Type: none
- Component Type: 0
- Foreign Priority: False
- Related Applications: ['13261814', '14936632', '13261813', '15611723', '15924253']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.582611020010967
- 35 USC 102 Novelty (BERT): 0.5462866415911851
- Combined Prediction Score: 0.5789785821689888
- Mean Citation Score: 444.90875
- Max Citation Score: 466.5781
- Similarity Product: 284.7924407591045

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

Dataset: test