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SAE ARP4102/8 - FLIGHT DECK HEAD-UP DISPLAYS Organization: SAE
Date: 1998-11-01
Description: This SAE Aerospace Recommended Practice (ARP) recommends criteria for the design and installation of Head-Up Display (HUD) systems. The recommendations are applicable to HUD systems for transport category aircraft, which display flight information (focused at infinity) in the forward field of view.
ARINC 764 - HEAD-UP DISPLAY (HUD) SYSTEM Organization: ARINC
Date: 2005-07-08
Description: Purpose: This document describes a Head-Up Display (HUD) system for installation in all types of aircraft.
SAE ARP5288 - TRANSPORT CATEGORY AIRPLANE HEAD UP DISPLAY (HUD) SYSTEMS Organization: SAE
Date: 2001-05-01
Description: The material provided in this document consists of recommendations related to the design, analysis, testing, and intended functions of head up displays (HUDs) for transport category airplanes. The content of the document is limited to statements of general design and installation considerations, including display function criticality and compliance considerations; symbology, coding, clutter, dimensionality, and attention getting requirements; equipment installation; display visual characteristics; failure modes; information display and formatting; specific integrated display and mode; and system verification.
SAE ARP5287 - OPTICAL MEASUREMENT PROCEDURES FOR AIRBORNE HEAD UP DISPLAY (HUD) Organization: SAE
Date: 1999-03-01
Description: This SAE Aerospace Recommended Practice (ARP) contains methods used to measure the optical performance of airborne binocular Head Up Displays (HUDs). This document covers methods for conformal and non-conformal HUD systems that are intended for use in the cockpit by the pilot or copilot.
SAE AS8055 - (R) MINIMUM PERFORMANCE STANDARD FOR AIRBORNE HEAD UP DISPLAY (HUD) Organization: SAE
Date: 2015-07-01
Description: This SAE Aerospace Standard (AS) specifies minimum performance standards for airborne binocular Head-Up Displays (HUDs) in fixed wing (14 CFR part 23, 25) aircraft; while this document is also applicable to rotorcraft (14 CFR part 27, 29) additional performance standards may be required for rotorcraft.
GMW16094 - HEADS-UP DISPLAY IMAGE STABILITY TEST - ISSUE 2; ENGLISH; GMW RESTRICTED/CONFIDENTIAL STANDARD – TO PURCHASE CALL 1-800-854-7179 USA/CANADA OR 303-397- 7956 WORLDWIDE Organization: GMW
Date: 2013-11-01
NTIS N8123798 - PRELIMINARY STUDY OF HEAD-UP DISPLAY ASSESSMENT Organization: NTIS
NTIS N8113636 - COGNITIVE ISSUES IN HEAD - UP DISPLAYS Organization: NTIS
NTIS N7933851 - THE ROLE OF COGNITIVE SWITCHING IN HEAD-UP DISPLAY Organization: NTIS
NTIS N8026296 - HEAD - UP DISPLAY IN THE NON - PRECISION APPROACH Organization: NTIS
NTIS N8123799 - A PRELIMINARY STUDY OF HEAD-UP DISPLAY ASSESSMENT Organization: NTIS
NTIS N7933201 - A REVIEW OF SOME HEAD - UP DISPLAY FORMATS Organization: NTIS
SAE/TP - 2009-01-3142 - HEAD UP DISPLAY PERFORMANCE IMPROVEMENTS AND COST REDUCTIONS THROUGH THE APPLICATION OF NON-CONVENTIONAL ENGINEERING SOLUTIONS Organization: SAE/TP
Date: 2009-11-10
Description: These improvements are not only in respect of size, weight, volume and cost for a given optical performance, but also in the characteristics that currently limit, or in some cases prohibit, the use of such displays in many cockpit applications. Displays that have been realized and tested through the implementation of these new techniques are described and their performance in laboratory and flight trials discussed, together with a discussion of the way ahead for further progress in their development.
SAE AIR4742 - DISPLAY CHARACTERISTICS OF FDI HEAD-UP GUIDANCE SYSTEM AS APPROVED FOR THE B-727 AIRPLANE Organization: SAE
Date: 2012-06-01
Description: The scope of this document is limited to descriptions of the display characteristics of the Flight dynamics, Inc. (FDI) Model 1000WS Head up Guidance System (HGS) as installed on the Boeing 727 airplane and certified by the Federal Aviation Administration for use in Category III landing operations.
NPFC - MIL-D-81641 - DISPLAY, HEAD-UP, GENERAL SPECIFICATION FOR Organization: NPFC
NPFC - MIL-D-70443 - DISPLAY UNIT, SIGHT, HELICOPTER HEAD UP SUBSYSTEM: M76 Organization: NPFC
NPFC - MIL-HDBK-87213 - ELECTRONICALLY/OPTICALLY GENERATED AIRBORNE DISPLAYS Organization: NPFC
Date: 2005-02-08
Description: This includes Head-Up Displays (HUDs), Helmet-Mounted Displays (HMDs), and Multi-Function Displays (MFDs), used for presentation of graphics as well as display of television (TV), forward looking infrared (FLIR), and radar video, and the associated electronic display generation equipment.
SAE AS6296 - ELECTRONIC FLIGHT INSTRUMENT SYSTEM (EFIS) DISPLAYS Organization: SAE
Date: 2016-03-01
Description: Functions that are not covered in this document include: Overspeed Warning; Air Traffic Control Radar Beacon System (ATCRBS)/Mode Select (Mode S); Automatic Dependent Surveillance - Broadcast (ADS-B); Traffic Information System - Broadcast (TIS-B); Electronic Map Display; Synthetic Vision; Enhanced Vision; Head-Up Displays (HUD); and Head Worn Displays (HWD).
SAE/TP - 2009-01-3144 - EVALUATION OF THE USE OF A HEAD WORN DISPLAY (HWD) FOR FLIGHT SUPPORT IN THE COMMERCIAL FLIGHT DECK Organization: SAE/TP
Date: 2009-11-10
Description: This study compared the performance of pilots flying a series of approach and landings under each of three conditions: using standard 737-NG flight deck displays only, using those displays with an optical head up display (HUD), and using those displays with a head worn display (HWD) depicting the same symbology as the HUD.
SAE/TP - 2009-01-3140 - OPTIMIZED SAFETY-CRITICAL EMBEDDED DISPLAY DEVELOPMENT WITH OPENGL SC Organization: SAE/TP
Date: 2009-11-10
Description: Historically, the majority of avionics display manufacturers have sought custom solutions to support the development of cockpit displays, head-up displays and other avionics on-board and ground displays, from specification through to target.

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