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A peer-reviewed article of this preprint also exists.
This version is not peer-reviewed
Submitted:
03 February 2023
Posted:
06 February 2023
You are already at the latest version
BERT | Bidirectional Encoder Representations from Transformers |
CFR | Code of Federal Regulations |
COND | Condition |
FAA | Federal Aviation Administration |
FAR | Federal Aviation Regulations |
GPT | Generated Pre-trained Transformer |
INCOSE | International Council on Systems Engineering |
LM | Language Model |
LOC | Location (Entity label) |
MBSE | Model-Based Systems Engineering |
MISC | Miscellaneous |
MNLI | Multi-Genre Natural Language Inference |
NE | Named Entity |
NER | Named Entity Recognition |
NL | Natural Language |
NLI | Natural Language Inference |
NLP | Natural Language Processing |
NLP4RE | Natural Language Processing for Requirements Engineering |
ORG | Organization (Entity label) |
RE | Requirements Engineering |
RES | Resource (Entity label) |
SME | Subject Matter Expert |
SOTA | State Of The Art |
SYS | System (Entity label) |
SysML | Systems Modeling Language |
UML | Unified Modeling Language |
ZSL | Zero-shot learning |
Serial No. | Requirements |
1 | The product shall be available for use 24 hours per day 365 days per year. |
2 | The product shall synchronize with the office system every hour. |
3 | System shall let existing customers log into the website with their email address and password in under 5 seconds. |
4 | The product should be able to be used by 90% of novice users on the Internet. |
5 | The ratings shall be from a scale of 1-10. |
Serial No. | Name of resource |
1 | Part 23: Airworthiness Standards: Normal, Utility, Acrobatic and Commuter Airplanes |
2 | Part 25: Airworthiness Standards: Transport Category Airplanes |
14 CFR §23.2145(a) | Requirements created |
Airplanes not certified for aerobatics must - | |
(1) Have static longitudinal, lateral, and directional stability in normal operations; | Requirement 1: Airplanes not certified for aerobatics must have static longitudinal, lateral, and directional stability in normal operations. |
(2) Have dynamic short period and Dutch roll stability in normal operations; and | Requirement 2: Airplanes not certified for aerobatics must have dynamic short period and dutch roll stability in normal operations. |
(3) Provide stable control force feedback throughout the operating envelope. | Requirement 3: Airplanes not certified for aerobatics must provide stable control force feedback throughout the operating envelope. |
Original Symbol | Modified text/symbol | Example |
§ | Section | §25.531 → Section 25.531 |
§§ | Sections | §§25.619 through 25.625 → Section 25.619 through 25.625 |
Dot (‘.’) used in section numbers | Dash (‘-’) | Section 25.531 → Section 25-531 |
Requirement Type | Definition |
Design | Dictates “how” a system should be designed given certain technical standards and specifications; |
Example: Trim control systems must be designed to prevent creeping in flight. | |
Functional | Defines the functions that need to be performed by a system in order to accomplish the desired system functionality; |
Example: Each cockpit voice recorder shall record voice communications of flightcrew members on the flight deck. | |
Performance | Defines “how well” a system needs to perform a certain function; |
Example: The airplane must be free from flutter, control reversal, and divergence for any configuration and condition of operation. | |
Interface | Defines the interaction between systems [62]; |
Example: Each flight recorder shall be supplied with airspeed data. | |
Environmental | Defines the environment in which the system must function; |
Example: The exhaust system, including exhaust heat exchangers for each powerplant or auxiliary power unit, must be designed to prevent likely hazards from heat, corrosion, or blockage. | |
Quality | Describes the quality, reliability, consistency, availability, usability, maintainability, and materials and ingredients of a system [63]; |
Example: Internal panes must be made of nonsplintering material. |
Original Interface Requirement | Modified Requirement “type”/category |
Each flight recorder shall be supplied with airspeed data. | The airplane shall supply the flight recorder with airspeed data. [Functional Requirement] |
Each flight recorder shall be supplied with directional data. | The airplane shall supply the flight recorder with directional data. [Functional Requirement] |
The state estimates supplied to the flight recorder shall meet the aircraft-level system requirements and the functionality specified in Section 23-2500. | The state estimates supplied to the flight recorder shall meet the aircraft level system requirements and the functionality specified in Section 23-2500. [Design Requirement] |
Requirements | Label |
Each cockpit voice recorder shall record voice communications transmitted from or received in the airplane by radio. | 1 |
Each recorder container must be either bright orange or bright yellow. | 0 |
Single-engine airplanes, not certified for aerobatics, must not have a tendency to inadvertently depart controlled flight. | 2 |
Each part of the airplane must have adequate provisions for ventilation and drainage. | 0 |
Each baggage and cargo compartment must have a means to prevent the contents of the compartment from becoming a hazard by impacting occupants or shifting. | 1 |
Requirement type | Training set count | Test set count |
Design (0) | 136 | 13 |
Functional (1) | 89 | 10 |
Performance (2) | 54 | 8 |
Total | 279 | 31 |
Requirement type | Precision | Recall | F1 score |
Design (0) | 0.80 | 0.92 | 0.86 |
Functional (1) | 0.89 | 0.80 | 0.84 |
Performance (2) | 0.86 | 0.75 | 0.80 |
Average | 0.85 | 0.82 | 0.83 |
Requirements | Actual | Predicted |
The installed powerplant must operate without any hazardous characteristics during | ||
normal and emergency operation within the range of operating limitations for the | 2 | 1 |
airplane and the engine. | ||
Each flight recorder must be installed so that it remains powered for as long as possible | 0 | 2 |
without jeopardizing emergency operation of the airplane. | ||
The microphone must be so located and, if necessary, the preamplifiers and filters of the | 2 | 0 |
recorder must be so adjusted or supplemented, so that the intelligibility of the recorded | ||
communications is as high as practicable when recorded under flight cockpit noise | ||
conditions and played back. | ||
A means to extinguish fire within a fire zone, except a combustion heater fire zone, | ||
must be provided for any fire zone embedded within the fuselage, which must also | 1 | 0 |
include a redundant means to extinguish fire. | ||
Thermal/acoustic materials in the fuselage, must not be a flame propagation hazard. | 1 | 0 |
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