Purpose: This document describes a Head-UpDisplay (HUD) system for installation in all types of aircraft. It describes the physical form factors, fit dimensions, electrical interface definition and typical HUD functions. The HUD system provides primary flight, navigation and...
This document recommends criteria for the design and installation of Head-UpDisplay (HUD) systems. The recommendations are applicable to HUD systems which display flight information focused at infinity in the forward field of view. This annex does not address devices...
This SAE Aerospace Recommended Practice (ARP) recommends criteria for the design and installation of Head-UpDisplay (HUD) systems. The recommendations are applicable to HUD systems for transport category aircraft, which display flight information (focused at infinity)...
This is a thorough description of this increasingly important technology, starting from the development of head-updisplays (HUDs), particularly specifications and standards and operational problems associated with HUD use. HUD involvement in spatial disorientation and its use...
The material provided in this document consists of recommendations related to the design, analysis, testing, and intended functions of headupdisplays (HUDs) for transport category airplanes. The content of the document is limited to statements of general design and...
This SAE Aerospace Recommended Practice (ARP) contains methods used to measure the optical performance of airborne binocular HeadUpDisplays (HUDs). This document covers methods for conformal and non-conformal HUD systems that are intended for use in the cockpit by the pilot...
This SAE Aerospace Standard (AS) specifies minimum performance standards for airborne binocular HeadUpDisplays (HUDs) in fixed wing aircraft. This document covers criteria for conformal and non-conformal HUD systems that are intended for use in the cockpit by the pilot or...
This SAE Aerospace Standard (AS) specifies minimum performance standards for airborne binocular Head-UpDisplays (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...
The scope of this document is limited to descriptions of the display characteristics of the Flight Dynamics, Inc. (FDI) Model 1000WS Headup Guidance System (HGS) as installed on the Boeing 727 airplane and certified by the Federal Aviation Administration for use in Category...
The scope of this document is limited to descriptions of the display characteristics of the Flight Dynamics, Inc. (FDI) Model 1000WS Headup Guidance System (HGS) as installed on the Boeing 727 airplane and certified by the Federal Aviation Administration for use in Category...
This handbook provides sample specification paragraphs, rationale, guidance, and lessons learned that are useful in the development of the primary flight displays and mission avionics controls and displays subsystem for an aircraft. This includes head-updisplays...