PATENT CLAIM ANALYSIS

Application Number: 16091667
Application Type: Utility
Filing Date: 2018-10
Publication Date: 2019-05
Patent Classification: ["235", "417000"]

Abstract:
A method and apparatus for generating, in an aircraft in flight, a feasibility display indicative of the feasibility of a weapon, the method comprising: providing a performance envelope for the weapon; determining, using the performance envelope, configuration data for configuring a generic algorithm; uploading the configuration data to the aircraft; generating feasibility data N indicative of the feasibility of a weapon carried on the aircraft successfully engaging a target and/or the feasibility of a weapon carried on the target successfully engaging the aircraft; determining, on board the aircraft, using the same generic algorithm and the uploaded configuration data, one or more test criteria; performing, on board the aircraft, an assessment process including determining whether or not the feasibility data satisfies the one or more test criteria; and, based the assessment, using the feasibility data, generating the feasibility display.

Claim (Index 11):
The method according to  claim 9 , wherein:\n the further generic algorithm is a generic polynomial; the further configuration data comprises coefficients for the generic polynomial; and determining the further configuration data comprises: acquiring a respective performance envelope for one or more different types of aircraft; using the one or more aircraft performance envelopes, determining a performance envelope defining the performance of all of the different aircraft types; using a weapon performance envelope and the performance envelope that is representative of the performance of all of the different aircraft types, determining a further performance envelope, the further performance envelope defining the weapon's performance when that weapon is implemented on each of the different aircraft types, the further performance envelope being the minimum envelope that defines the weapon's performance when that weapon is implemented on each of the different aircraft types; and determining the coefficients for the generic polynomial that fit the generic polynomial to the further performance envelope.

Metadata:
- Claim Count in Document: 35.0
- Percentile: 97.0
- Lexical Diversity: 2.78947
- Patent Class: 235.0
- Transitional Phrase Type: none
- Component Type: 0
- Foreign Priority: True
- Related Applications: ['15037367', '13389979', '13370195', '11990615', '14551622']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.5521622654650915
- 35 USC 102 Novelty (BERT): 0.5278588990572725
- Combined Prediction Score: 0.5497319288243097
- Mean Citation Score: 218.504632
- Max Citation Score: 362.85568
- Similarity Product: 264.09298625823976

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