F-16 Head-Up Display

Similar documents
aerofly FS 2: Rodeo s Tutorial My second ILS approach

EasyFMC. - Documentation -

Pilot s Operating Handbook Supplement AS-04

ILS APPROACH WITH B737/A320

FSXmap.com. Interactive Airport and Runway map for Flight Simulator X

VFR Module 2. G1000 Transition VFR Module 2

AVIATION MERIT BADGE

Counselor s Name: Counselor s Ph #: 1) Do the following: a) Define "aircraft." Explain the operation of piston, turboprop, and jet engines.

Single Engine Instrument Training Record I PREFLIGHT PREPARATION WEATHER INFORMATION weather reports and forecasts. pilot and radar reports.

USE OF RADAR IN THE APPROACH CONTROL SERVICE

FlyRealHUDs Very Brief User s Manual

AIRBUS FlyByWire How it really works

EXPERIMENTAL STUDY OF VERTICAL FLIGHT PATH MODE AWARENESS. Eric N. Johnson & Amy R. Pritchett

This is the fifth of a series of Atlantic Sun Airways CAT B pilot procedures and checklists for our fleet. Use them with good judgment.

Instrument Proficiency Check Flight Record

Mastering ILS Approaches

OPERATIONS CIRCULAR 01/2012. Subject: HEAD-UP DISPLAYS (HUD) AND ENHANCED VISION SYSTEMS (EVS)

1.- Introduction Pages Description 21.- Tutorial 22.- Technical support

OLM FBW 2006 Toulouse September Head Up Display

Date Student Name Instructor Aircraft Make and Model Time in Aircraft Initial score corrected to AHRS: ADC: TIS: Terrain: TRK: DTK: VNAV:

APOLLO GX50/55 GPS IFR Operations

General Characteristics

Scout s Name: Unit Number:

ultimate traffic Live User Guide

GENERAL INFORMATION Aircraft #1 Aircraft #2

HARD. Preventing. Nosegear Touchdowns

REPORT SERIOUS INCIDENT

This is the third of a series of Atlantic Sun Airways CAT A pilot procedures and checklists for our fleet. Use them with good judgment.

MODEL: ELITE AATD RC-1

del Airbus en el mundo de la

Private Pilot PTS. FAA-S B Private Pilot Practical Test Standards For Airplane (SEL, MEL, SES, MES) November 2011 (Effective June 1, 2012)

COMMERCIAL LEVEL SIMULATIONS

Garmin 500 Checkout. Addendum to Aircraft Checkout Form

AIRCRAFT ACCIDENT REPORT AND EXECUTIVE SUMMARY

A Hong Kong-based Virtual Airline. Hong Kong VFR Guide. VOHK Training Team. Version 1.2

UPDATE ON THE 6 IDEAS (1-4) NAV CANADA

KSFO RNAV TO GLS DEMONSTRATION

Aviation. Unit: Counselor s Name: Counselor s Ph #: 1. Do the following: a. Define "aircraft." Explain the operation of piston, turboprop,

TCAS Pilot training issues

Airbus A V Speeds and Ranges. Speed Limits

NATIONAL PILOT LICENCING

FIRST FLYING TECHNIQUES - APPROACH AND LANDING


NATIONAL PILOT LICENCING

Dive-and-Drive Dangers

Cessna 560 Citation, D-CAUW

FLIGHT OPERATIONS REQUIREMENTS AEROPLANE APPENDIX 8. FLIGHT RECORDERS

Operational Benefits, Affordability and Availability

Aviation Merit Badge Workbook

US Navy virtual Basic and Advanced Instruments for FS2004. By Marcel Hendrikse

FLIGHT STRIP MANAGEMENT - APPROACH LEVEL

GENERAL REVIEW & PREFLIGHT TEST

ACCIDENT. Aircraft Type and Registration: Airbus A , G-EZFV. No & Type of Engines: 2 CFM56-5B5/3 turbofan engines

HEAD-UP DISPLAY (HUD), EQUIVALENT DISPLAYS AND VISION SYSTEMS

1973 Cessna Skymaster 337 Instrumentation

Integrated Flight Instrument Systems

MetroAir Virtual Airlines

INTERNATIONAL VIRTUAL AVIATION ORGANISATION CANADIAN AIR TRAFFIC CONTROL PHRASEOLOGY ATC OPERATIONS DECEMBER 2016 BY: MATHIEU LAFLAMME

Navigation - Runways. Chap 2, Nolan

Indiana State University Aerospace Technology

IFR SEPARATION WITHOUT RADAR

Scenario Training VGT - IWA

2007 Instrument Procedures Handbook; Chapter 5 Approach

2018/09/01 05:24 1/1 Flight Plan

Instrument Multi Engine Practical Test Standards

Approach-and-Landing Briefing Note Response to GPWS Pull-Up Maneuver Training

This page intentionally left blank.

COPYRIGHT NOTICE Copyright 2010 Honeywell International Inc. All rights reserved. All marks are owned by their respective companies.

Instrument Proficiency Check

Head-up Guidance & Vision Technologies Enabling Safer and More Efficient Airline Operations

Detailed information on the flight computer/calculation functions are also described in detail below.

Garrecht TRX 1500 Traffic-Sensor

The SESAR Airport Concept

Canadair Regional Jet 100/200 - Automatic Flight Control System

Instrument Rating Syllabus

GACE 2017 GROUND TEST NAME DATE SCORE CHECKED BY: DATE CFI# Circle the correct answer or write in where applicable. Test will be corrected to 100%

LESSON PLAN Introduction (3 minutes)

Aerial Photography and Flight Planning

Investigation Report

Khartoum. Close Call in. causalfactors. Confusion reigned when an A321 was flown below minimums in a sandstorm.

AVIATION INVESTIGATION REPORT A06Q0180 LOSS OF ELECTRICAL POWER

Chapter 6. Nonradar. Section 1. General DISTANCE

How to Program the PMDG 737 NGX FMC

AVIATION OCCURRENCE REPORT A98W0216 LOSS OF SEPARATION

FLIGHT OPERATIONS PANEL

McDonnell Douglas MD-81 registered OY-KHP Date and time 6 February 2010 at 18h25 (1) Operator

AUTOMATIC FLIGHT MANAGEMENT SYSTEMS TABLE OF CONTENTS

The aim of any instrument approach is to allow the aircraft to safely descend to a low altitude in order to become visual.

Lesson: Descent Control

Flight Evaluation Schedule For GPS IFR Approval Primary Means Enroute, Terminal and Non-Precision Approach

International Journal of Innovative Research in Advanced Engineering (IJIRAE) ISSN: Issue 11, Volume 5 (November 2018)

Advisory Circular AC61-3 Revision 11 SUPERSEDED Define and identify, on a diagram of the earth, and explain the meaning of the following:

Using The Approach Planner

AIRCRAFT ACCIDENT REPORT AND EXECUTIVE SUMMARY

Virtual Royal Air Force 208 (R) Sqn Syllabus

Gleim Instrument Pilot FAA Knowledge Test 2015 Edition, 1st Printing Updates April 2015

R9 Slides - Systems & Limitations Validation Questions

TRANSPORT CANADA MMEL SUPPLEMENT PIPER AIRCRAFT PA-31, PA , 325, 350 MASTER MINIMUM EQUIPMENT LIST

BFC KNOWLEDGE TEST. 4. What are wing-tip vortices (wake turbulence)? With which aircraft are they the greatest? Describe proper avoidance?

02.00 Page 1 A320 ELT COURSE. FNPT 1...Page 1 FNPT 2...Page 3 FNPT 3...Page 5

Transcription:

F-16 Head-Up Display Discover a new way to fly... Keep looking outside while flying the F-16 at high speed and low altitude. Layout The HUD information layout is shown on the images below, in 2D panel view and in full-screen view.

All the necessary flight information is displayed on the HUD so that you can fly the aircraft while looking outside: The airspeed is displayed (in knots) with a speed tape and the current value The barometric altitude (in feet) with a scrolling tape and the current value The magnetic heading with a tape and the current value The flight path vector The radio-altitude (in feet), which is the height of the aircraft above the ground level Navigation information Target designation box, if the radar is installed Alert messages The load factor (in G) The Mach number The bank angle Expert users might be interested in learning how to integrate this HUD in any panel. This section is dedicated to people who know how to edit a panel though the panel.cfg file. If you think you can do this, have a look at the HUD integration section at the end of this document.

Flight path vector This is definitely the most important part of the HUD. Unlike classic aircraft instruments, such as the attitude indicator and the compass, the flight path vector shows exactly where the aircraft is flying. You can fly the aircraft through its trajectory. When the flight path vector is above the synthetic horizon, the aircraft climbs. If it is below the horizon, the aircraft descends, even if the nose is above the horizon. The flight path vector is accurate and refreshed in real-time. Low-Level Flight On these images of a low-level flight, the flight path vector is positioned just above the mountain top to make sure the aircraft will fly over the mountain and not crash into it. As long as the flight path vector is maintained above the mountain, the aircraft will fly over the mountain. The flight path vector is maintained above the mountain, the aircraft will fly over the mountain Low-level flight is easy, even at very low altitude. See the radio-altimeter: 114 feet. Outside view: the aircraft is flying at very low altitude. Easy...

Landing with the HUD When the landing gear is extended, the HUD automatically switches to the landing mode. The heading indicator is moved to the upper part of the display and a new symbol appears: the landing incidence guide. It shows the range of correct incidence for landing. You should maintain the flight path vector within this range to make a perfect landing. When the aircraft is in landing configuration (gear extended, flaps and slats deployed, airspeed around 150-180 knots), the flight path vector has just to be aligned with the runway entry to guide the aircraft to landing. The sequence shows an almost perfect landing using the HUD flight path vector and incidence indicator: The flight path vector is positioned on the runway entry and it is in the correct incidence range. The aircraft is on the glideslope, perfect. As the aircraft gets closer from the runway, it is a little low on the glidepath, but the flight path vector is still aligned with the runway and the incidence is good. The flight path vector is maintained in the right incidence range, still aligned with the runway. The airspeed is a little low, but still good. The touchdown is very close. The flight path vector shows the aircraft will touch the ground at the very beginning of the runway. Easy with a good HUD... The HUD can show when the landing is not going right: The flight path vector is positioned BEFORE the beginning of the runway. The aircraft will not land safely... The flight path vector is above the incidence range indicator and the speed is too high. Managing Cross Wind The HUD lets you see visually the wind drift caused by the cross wind. The flight path vector and pitch ladder move laterally to show exactly where the aircraft is flying, so if they move to the right, it means the aircraft is "pushed" on the

right by the wind that comes from the left. The wind coming from the left pushes the aircraft on the right. The flight path vector and pitch ladder are shifted to the right. Using the HUD, cross wind landings become easy after a little training. Even if the wind is strong, you just have to keep the flight path vector aligned with the runway: This landing sequence shows the aircraft is flying in the direction of the runway even if the nose is not heading to the runway. This is easily managed with the HUD flight path vector. The landing is not perfect because the flight path vector is not in the correct incidence range. The approach descent is too flat and the speed is too high, but this is safe when the wind is blowing.

Navigation Information If a flight plan has been entered or loaded in the GPS, the HUD provides navigation information to fly to the next waypoint. The bearing and distance to the next waypoint are displayed. A diamond shows the direction of the next waypoint, if it is in sight. If no flight plan is defined, the bearing and distance are blank. Target Designation Box The radar developed by Eric Marciano must be installed to enable this feature. The target designation box shows the direction of the target selected on the radar (even if the target is too far to be visible) and the distance to the target (in NM), below the box. It allows you to fly yor aircraft to the target for interception. When the distance to the target is less that 1 NM, the distance stops being displayed.

The target is at 27.2 NM, beyond visual range. The flight path vector is aligned with the target designation box to fly directly to the target. At 3.8 NM, the target is hardly visible (the contrails are visible), the designation box shows the direction. At less than 1 NM, the distance information disappears. The target is now visible. The target designation box is active as long as a target is selected on the radar. If you unselect the radar target, the box disappears. Alert Messages The HUD displays alert messages when needed, such as the warning message shown on the image below. The possible messages are: WARN: This message means you are flying too low, or your descent rate is too high according to your current altitude. Anyway, you should pull up the stick. FUEL: the fuel quantity on board is too low. You should land very shortly.

The altitude is low and the aircraft is descending. It triggers a warning message. F-16 HUD Integration The best way to understand the HUD panel integration is to see how it is integrated in the F-16 panel. The integration is exactly the same in FS2004 and FSX. Basically, the HUD is an XML gauge that is listed in the panel.cfg just like any other gauge. In fact, the HUD provided here has 2 gauges: 1 for the 2D/3D panel integration and 1 for the full-screen usage using the "mini-panel" feature of FS2004/FSX. In order to have the HUD showing in a panel, edit the panel.cfg and use the following gauges: F16_HUD!Main for the 2D panel or Virtual Cockpit F16_HUD!Full for the mini-panel, designed for the full-screen HUD Keep in mind that the F16_HUD.cab file must be in the panel directory if you want to have the HUD working. Here is the example of the F-16 panel: gauge00=f16_hud!main, 353,35,320,330 Just like for any other gauge, the HUD is positioned at 353,35 and its size is 320 by 330. The HUD full-screen integration uses the mini-panel feature of FS2004/FSX. This is why it must be integrated in a separate panel window which identifier is MINIPANEL. Here is how it is done in the F-16 panel: [Window09] position=8 size_mm=1024,768 child_3d=1 background_color=0,0,0 ident=minipanel gauge00=f16_hud!full, 190,35,644,660 The [window09] section defines this window as a mini-panel, which includes the HUD in full-screen mode. Consequently, the HUD will appear in full-screen when you press the W key. Pressing the W key switches the panel off, which makes the mini-panel appear. Pressing W again switches the mini-panel off, and pressing W again brings the panel back. For more information about the integration of gauges in a panel, please refer to the Microsoft Panel SDK.