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From SAE International, SAE MobilityRxiv is a free online preprint server and sharing service for English-language preprints in the mobility/transportation field

Applicable to SAE Level 3, 4, 5 ADS-equipped vehicle value chain (development, manufacture, operation, and decommission). Inclusions: Any development, manufacture, and deployment of ADS technology such as On-road personal- or fleet-owned and operated passenger motor vehicles, Transportation as a Service (TaaS), Mobility as a Service, taxi, delivery, shuttle vehicles, trucks, and buses, and enabling or supporting services. Exclusions: Off-road or closed course applications (e.g. mining, on airport, industrial equipment).

This SAE Recommended Practice provides definitions, taxonomy, and characteristics for DA metrics used to quantify the driving performance of ADS-operated vehicles. Here, the primary focus is on the safety-related driving performance, which is considered to be related to completion of the dynamic driving task (DDT) . Driving performance is a subset of overall operational performance of ADS-operated vehicles. Thus, assessments of cybersecurity, maintenance, interactions with passengers, etc., while important, are out of scope for this document. Note that the DA metrics do not specify the actions and/or maneuvers to be executed by the subject vehicle. A literature review of DA metrics that have been proposed and, in some cases, used in previous studies was conducted. From this literature review, a set of DA metrics has been created with example usage. Evidence of prior research indicating that a metric has a relationship with safety outcome(s) is included where applicable.

This SAE Recommended Practice provides guidance for test facilities in identifying potential hazards, and safety risks, along with requirements and recommendations related specifically to testing of automated driving systems (ADS) and ADS-operated vehicles. Herein after, for the purposes of this document, utilization of the term “test facilities” implies those conducting testing of ADS or ADS-operated vehicles, unless otherwise noted. References made to safety within this recommended practice apply only to test method safety and driving safety on and during testing at an ADS test facility and do not apply to vehicle design or safety performance. Safety practices for on-road testing, operation, and related deployment are not covered within this document.

This standard establishes the minimum navigation system performance requirements for UAS medium risk specific assurance and integrity level operations.

The scope of information desired includes any information relative to how a Electrical, Electronic, Electromechanical, or Electro-Optical piece part is produced. This data might include business approaches to releasing product, to manufacturing operations and controls, to testing philosophies, to actual piece part data.

The scope includes Military Standard screening and qualification testing for all active EEEE part types. Scope may be expanded to include passive EEEE devices at a future date.

This Aerospace Standard establishes the diameter-pitch combinations of ISO metric 60° screw threads recommended for use in the aerospace industry for metric module bolts and nuts.

This standard establishes the minimum navigation system performance requirements for UAS operation within a specific use case.

This document is intended for use during audits to the requirements of AS5553C. It may be used by all contracting organizations that procure EEE parts, whether such parts are procured directly or integrated into electronic assemblies or equipment as guidance for evaluating compliance to AS5553C.

This white paper is an examination of the increasing rate of injuries and deaths worldwide of a class of road users, often referred to as “vulnerable road users” (VRUs), with a focus on pedestrians, cyclists, scooterists, highway road workers, safety, and emergency personnel. The potential to leverage pragmatic, evidence-based technology countermeasures to reduce these collisions, and the severity of those that do occur, is also examined.

The SAE Recommended Practice establishes minimum performance requirements and related uniform laboratory test procedures for evaluating lateral (curb) impact collision resistance of all wheels intended for use on passenger cars and light trucks.

This SAE document defines a recommended practice for implementing circuit identification for electrical power and signal distribution systems of the Class 8 trucks and tractors. This document provides a description of a supplemental circuit identifier that shall be utilized in conjunction with the original equipment manufacturer’s primary circuit identification as used in wire harnesses but does not include electrical or electronic devices which have pigtails. The supplemental circuit identifier is cross-referenced to a specified subsystem of the power and signal distribution system identified in Section 5.

This SAE Recommended Practice establishes the antilock brake system (ABS) sensor interface and envelope dimensions for standardizing the location of the ABS rings mounted on or integral to the inboard end of spoke wheels, hubs, rotors, and hub-rotor assemblies on the following axle designations as defined in SAE J1842. a FF b FL c FC d FH e L f R g U h W j N k P

The range of test conditions on the dynamometer shall be sufficient to determine the primary operating characteristics corresponding to the full range of vehicle operations. The characteristics to be determined are: a Torque ratio versus speed ratio and output speed b Input speed versus speed ratio and output speed c Efficiency versus speed ratio and output speed d Capacity factor versus speed ratio and output speed e Input torque versus input speed NOTE: For more information about these characteristics and the design of hydrodynamic drives, refer to “Design Practices: Passenger Car Automatic Transmissions,” SAE Advances in Engineering, AE-18 (Third Ed.) or AE-29 (Fourth Ed.).

This Aerospace Standard covers all automatic pressure altitude code generating equipment manufactured under this standard and complying with the requirements specified herein up to the maximum range of pressure altitude as indicated on the equipment nameplate. In those cases where the code generating equipment forms part of an aircraft system, such as a pressure altimeter, an air data computer or an ATC Transponder, this standard applies only to the code generating equipment as defined in paragraph 1.2.