we -al t hlc lfmuimsmileand will contain 6-4e word lommon to thes.e modes. the only further...

Post on 26-Jan-2020

0 Views

Category:

Documents

0 Downloads

Preview:

Click to see full reader

TRANSCRIPT

AD-A022 655

HEAD-UP DISPLAY SYMBOLOGY

William P. Orrick, Jr., et al

Naval Air Development CenterWarminster, Pennsylvania

31 December 1975

DISTRIBUTED BY:

We -al T" hlc lfmuimSmIleU. S. OEPMlliDIT OF CSINICE

DISCLAIMER NOTICE

THIS DOCUMENT IS BEST QUALITYPRACTICABLE. THE COPY FURNISHEDTO DTIC CONTAINED A SIGNIFICANTNUMBER OF PAGES WHICH DO NOTREPRODUCE LEGIBLY.

ftEOWV N. NAMM-75267-40

HEAD-UP DISPLAY SYMBOLOGY

14DWilliam P. Orrick, Jr., arid Phyllis E. York

0 Craw Systems DepartmentCQ NAVAL AIR DEVELOPMENT CENTERo ~Warminster, Pennsylvanti 18974

31 December 1975

PHASE REPORTAIRTASK NO. A34(4'JO0O/OOIC/6WP30201 ~ l

Work Untt WF55-525-402

APPROVED FOR PUBLZC RELASE; DISTRIBUTIO E UNLZIXTED.

Prepared for INAVAL AIR SYSTEMS COMMANND

Department of the N,.yWashington. 0. C. 20361

NATIONAL 'ECIiNICALINFORMATION SERVICE

UI.S. DEPARI MENI OF COMMERCESPRINGIIFLU. VA. 21161

-%k

:IOT ICE S

ntep" I NUu~wfItgs Im" - 7%lam 16M N f ad" NEW~s pIUIp6wa bo by Sw N~d Aira .We C is 1W" IS ~IM WI iW~ Ma lpde I0WL go*m fmol eVdev , .,4000 .Molyw 0 sM so ý- w in. mud * tow Ali 2*1 mlsum smg udos"*n No0w"fW 00w"WiFwaim MWA ~ n vmpswul, 100w mam orft L Po p -us RspI NOiD 1EAM73034-4 hidulini

W M 01s Is IWO for' *0 vow 102 OWd ps w by *a Craw N3p~m s Pflu.. "he

caGE UfFlM ON DIPARTIENT

00 CsMKMmn. N"d Air Owdopswnt CMr 101 TftWmIW bkofter, Nod Air IWOuWMsW CmWW

ol Prapso WMA FkWm~ M-1 MnW II D@Psuhinn04 PtAWWW h SWOM Prapam WOM

* OS Uup mud Air go son- MogwtSin Piapgom Offi Iof Tsoili Air WkrtmOW.

10 Nod Air Fw.ifty Wwmlnomr2a Awee flocums Tedwuou Dopwuwram30 Air Vbide TedwlwMv Depstmsna40 Cm 2 Smwm Odpwv.maso --n. Arudyle eli Erlewor~ng Deparimnm

w "W- kw m Oumnnusi

PAOOUCT ENDORSEMENT The dmugsion or jructktm amcon~uivi etjwnwtwci product hirim do"III cosfhlhs~ an evoumsmo by the Gwmwrnment ner do they cowey or Imply ow license or right to usewch produicts.

FTIf WIit 4flca

APPROVED BY 044-l.6- DATE:-JLLJL 7L-H. BLACKDUM, CAPT. M4C, UJSN

UNCLASSIF-:D,.ZZURITY CLASSIFICATioto OF THIS P-AaE (*%, on DaaRbfte.4h

REPORT DOCUNENTATIOt4 PAGE Z DtUT s

rierl 7GOVT IEMO PO ICINISVI11 CA TAEZLO 40

NADC-7.;267-40

HIIAV-UP DISPLAY SYMBOLOGY 13 May 7S - 12 June 75PS. PMV@RssNG 0414. P42POPIT NURSER

r7 AU~TiDft(.) 0. CONTRAC 7OR GRANvT h.mUEfd'

Killian P. Orrick, Jr.

f pIERIPORuMpb ORGANIZATION MAMIE AND AGGRIESS -I.P~9fAEI,1 a fq~ET TAUNCrew Systems Department (Code 4022) AWAIMASWOUNI NUMuEN

Naval Air Development Center A3400000/00IC/6WPN02001Warminster, P'ennsylvmnia 18974 Work Unit 0P55-525-*402

I I. C:ONTROLLING OPPICE NAMIE AND ADDRESS 11. REPORT OATS

Naval Air Systems Commnand 31 Dec 1975Department of' the Navy ?1. NUMBER OF 'WAGES

14 ORR -AI mm.eWlr ~a)t.U MT CLASS rotlh' 01G.. ra' in

IS. DISTRfOUTION STATEMENT (.1Gat Ifleperl)

APPROVED FOR PUBLIC RELEASE; DISTRIBUTION UNLIMITED

IT. DISTRINUTION STATIEMENT fel $he altactl alaftm4 O Bleak it II ltmont heat R~epor)

IW S.JPPLEMIENYARY NOTES-

IV. KEY WORDS (CeaeW.. ow rawm.. side it naeassav smd ismlIlj' br bleuk rm~wh)

* Visual displaySymbolog~y

IF Head-up display

20.ANSTIRACT (C..ithow o ever siO de It nemeaspoy meNJolt fdnIf by l*i uua)

This report consists of a table and acco~anying illustrations which de-scribe aircraft and weapons system functions displayed on the head~-up dis-~plaiys in the A-7E, F-5, F-14, F-iS, F-lilA, CL-84, and AV.-8A aircraft.Corresponding display formats as given in MIL-D-8i641(AS) and MIL-Sllh-884Bare included for comparison.

DD IJAORM 1473 RDITIO00 OP? I NOV 46I 19 GNOLETEK I

ISECURITY CLASSIFICATION OF T1I419 ,Ifl.~~l.d

NAIK:- 75267-40

TABLE OF CONT UNTS

Page

INTRODUCTION . . ... . .. .. . . . . .. .. . . .. . 2

DESCRIPTION OF THE TAIES ..................... .................. 2

CONTENTS OF TABLES .......................................... . 4

TABLES ..... ....... ....... ........................... ... 12

FIGURES ................... . ............................ ... 56

MODES ..................... .............................. .. 72

LIST OF ABBREVIATIONS ............. ...................... 73

REFERENCES ................ ............................ .. 75

.....

-- . . ._. . .. . .1 . .. . .,.- . ....... ...... ___ ___

NAD.- 15267-40

I N T P. 0 1) II C 1 0 N

The head-up display (HUD) was developed to facilitate the transition be-tween Instrument and visual flight. The use of a IUD is becoming increasinglyCommon. In spite of the existence of a Military Specification and a MilitaryStandard which are written to promote consistency and to minimize occurrence

of incompstible methods of presenting information, inconsistencies do exist.The follkwin'g tables were prepared in order to facilitate comparison betweenexisting head-up d:•.splay formats, so that In the selection of symbols for fu- i

ture heia-up displays inconsistencies will be minimized,

The tables included in this report contain data on displays found in theA-7E, F-5, F-14, F-IS, F-=IlA, CL-84, and Al-BA aircraft. Data from the Mil'•-tary Specification pertaining to head-up displays, MIL-D-.81641(AS), and the Vrelevant Military Standard, MIL-STD-8584 are included. The information in thetables was taken from the references listed. Where available, the NATOPS Man-ual (U.S. Navy) or Technical Orders (USAF) were considered the primary source.Information from secondary sources was included in the tables where it indi-cated additional functions or alternative ways of displaying the same ftnctions.

D E SCR I PT I ON OF THE TABLES

Descriptive parameters are listed at the left edge of the tsbles. Func-tions are listed across the top edge. Functions are presented alphabeticallyand are consecutively nmbered. Where there is more than one means of display-ing a fwiction for a given aircraft, additional columns are used. The functionname is the same, and the same number is used with the notation "(cont)" to in-dicate continuation of the description. Explanation of the parameters, as nec-essary, is given below. Blanks in the body of the tables indicate that theparameter is not relevant or the required iniformation was not available.

Function - In general, displays present standard aircraft or weapons in- iformation and the function names reflect this. There are two types of excep-tions. One is where a function is peculiar to an aircraft; e.g., wing sweep in

the F.-14,, The other exception concerns functions without qualifying adjectiveswhere there should be a qualifier. An example is the use of the term "ai-r-speed" without the accompanying "indicated," "true" or "calibrated." In suchcases, a separate heading without the qualifier was included in the tables.

Figure No. - Refers to the figure which shows the display elements as du-scribed in the ables. In order to limit the number of figures, references aresometiimes made to a figure shd ting a display similar to but not identical informat to the display described. For example, the number of scale graduationsor intervals may be different, but the relationships among scale marks, nu-,merals, pointers and labels are the same. It is possible to determine fromthe table entries and the figure how the display looks. Numerals in circleson the figures refer to the function nmaber in the tables. Arrows fr,•m •,•csoenci-Pled nv,,rals point to display elements which are used for the function

-2

S. . . . - - -=

NADC-75267-40

whose number is given. Sometimes a figure number i.% given In a table entryfor a function and the number of that ftmcti,ýn does not appear on the figure.This is either because the figure portrays only that function, the figure isself-explanatory or the relationship -.s v.or Y,.•ely •xplained in the notes forthat function. In sor cases, one of the eo•,• c•o.W,tions holds yet there isa numeral on the figure. This is due to n cnservative nature of the au-thors' approach.

Forn of Display - The components of a fuwctional display, as shown in the Icorresponding figure, were classified as sqalos (vertical, horizontal, or cir-cular), ladders, digits, letters, alphanum.irics, or symbology.

Display Label - Any letter(s) used to label the display are indicated. Tnthe corresponding figure, a single letter has been drawn to indicate the posi-.tion Gf a single letter label; two letters have been drawn to show the positionof a double letter label. In each case, the letter(s) in the actual label maydiffer from those used in the figure.

Range of Variable - The range of parameter values which may be displayedis given.

Range Displayed - The range of parameter values which is displayed at agiven time is indicated.

Direction of Increase - The direction of increasing parameter values isgiven in relationship to the appropriate scalar display. For a vertical scale,parameter values increase as one reads up the scale, down the scale, or both;for a horizontal scale, values increase as one reads to the left, to the right,or both. For a circular scale, values increase in a clockwise or a counter-clockwise direction.

Fixed Scale - "Yes" indicates the scale remains stationary; "no," thescale acts as a moving tape.

Scale Values Marked - "Yes" ti licates scale graduations are labeled withnumerals to indicate parameter vaT )s.

Scale Graduations - The change in parameter value for the smallest grad-uation on a scale is given.

Moving Reference - "Yes" indicates a reference mark clhanges its positionon the screen in some manner.

Modes - With certain exce:itions, modes are listed as named in referencesources (see mode list). In cases where the table entry does not correspondexactly to the mode list, the table entzcy wili encompass more than one modeand will contain 6-4e word Lommon to thes.e modes. The only further exceptionis the use of the word "attack" to include all modes in the A-71T' where a weaponis used.

Notes - When a functitn description has been obtained from a secondaxyreference source (reference 4 or reference 6) this is indicated by inclus!onof the source number in the "notes" section.

"H .. .• ... .I I I Ill • I. . ....I .. .. ..... . . . .. .. . .. . ., ... ... •- : --.. _- -

MADC-75267-40

CONTENT S OF TAR LES

FUNCTION TABLE ENTRY FIGURE

Acceleration Display (Lateral)CL-84 ...... . . . .. . . ........ 1AV-8A 2... ........ 2 50

Acceleration Display (Vertical)A-7 I....... . . ......... 3 2F-14 . . . . .. . ....... . 4 3

Acceleration Limit DisplayF-S .... . . ...... ..... 5 4

Airspeed CommandF-15 . . . . . . . . .S

CL-84 .......... . .. . .... 7 1AV-SA .... . . .......... . 6MIL-D-81641(AS) ........ . . . .. . ...... 9 5MIL-STD-884B ........ . . ......... 10 5

Airspeed DisplayCL-84 . .. . . . . 1MIL-D-81641 (AS) .... . . ...... ...... 12 5MIL-STD-884B. .. . . . ............ 13 5

Airspeed Display (IAS)A-7 ........ . . ......... . 4 7F-14 ...... . . .. . . ......... 15 3F-IS ...... .. . ......... 16 5AV-8A .......... . ......... 17

Airspecd Display (TAS)AV-8A ............ . .. . ..... 18

Air-To-Air Attack Steering DisplayF-A4 . . . . . . . . ... 198

9H F-A410

F-IS . .................... . 20 12

Air-To-Ground Attack Steering DisplayF,-14 .. . .... ............ 21 13

9F-15 ........ . .......... . 22 14F-1lIA .......... . ........ 23 is

Altitude CommandF-14 ...................... 24 16F-15. . . 25 17MI .-D-.81641 (AS) . .................. 26 17

MIL-STD.-B84B .. . . . . . .......... 27 17

-4--bL~t g • .*v • "" .. .. . - .

NADC-7S267-40

CON~TENTS 0 F T AB L ES (coxit,"ý.ued)

FUNCTION TABLE ENTRY FIGURE

Altitude Display (Barometric)A-7 . .. .. . . 23 16F-14 . ...... . . .......... 29 18F-IS16F- . . . . . 30 17

AV-SA .. . . . . . . . .. 317MIL-D-81641(AS) ........ . . ......... . 32 17MIL-STD-964. ........ . . ........ 33 17

Altitude Display (Radar)A-7 ............... 34 16F-14 . .. .. .5 18 .

16CL-84 .. . . . . . 36AV-8A..... ..... . 37MIL-D-81641(AS) ........ ... 38 17MI1L-STO-884B ...... . . ......... . 39 17

Angle of Attack DisplayF-15 . . . .. . . ....... . 40 5AV-8A ................ 41 19

Angle of Attack Error DisplayA-7 ........ . . ......... 42 20F .I I ....... . ........ 43 21

20MIL-D-81641(AS) ...... . ........ 44 21MIL-STD-884 . . ... . . ......... 45 21

Angle of Attack (Optium) DisplayF-IS .. ... ... .. 46 5

Armament Datum Line DisplayF-14 ............. 47 22F- 15 ........ . . ...... .. 48 22AV-8A............ 49 22MIL-D-81641(AS) so...........5 22MIL-STD-8841 . . . . . . . . . . . 51 22

Armament So ection DisplayF-14 ........ . . ......... 52MIL-D-81641(M ... . .. ... ....... 53F-S .. . . . . . ......... 54MILl-STD-884. ........ . . ........ 55

Attitude DisplayF-1i4 ..... ... ... ... .. 56 23

26

.Jam~ w~i ' • ....- • ........ " i • • -. = -

NADC-75267-40

C 0 N T E N T,'; O F T A L E1S (E o n t i n u e d)

FUNI•NIOI TABLE ENTR'Y FIGURE

Attitude Display (Continued)F-is ...... . . .. . . ......... 57 25F-IlIA I... . ....... .. 58 15CL-84 .. . . ......... 59 1AV-8A ........ . . ......... 60 27

-D-.31f . . . .. . . . . . . 61 26NIL LSTD-884B .. . . . . . . . . . 62 26

Bank Aigle CommindF-14 ...................... 63 28

Bomb Fall Line DisplayA-7 ........ . . ......... 64 13F-14.. ....... . . . 65 13F-IS ........ . . ......... 66 13MIL-D-81641 (AS) .. . . .. . .......... 67 13MIL-STD-884B .......... . . ..... . . 68 13

Breakaway CommandA-7 ............ . .. . .. 69 29F-14 ............ . . .. . 70 29F-is .......... . . ...... 71 29AV- 8A .......... . . ...... 72 2-9MIL-D-81641(AS) ........ . . .... .... 73 29MYL-STD-8848... ... . . .......... 74 29

Closure Rate ComandM L-D- 1641 (AS) .......... . ......... 75 17

Closure Rate DisplayF-14 .......... . .. . .... 76 30

55F-.15 .... . . . .... ...... 77 56MIL-D-81641 (AS) ........ . . . .. . ...... . 78 17MIL-STfO-884B .... . . ............. 79 17

Course ConwindA-7 .......... . ......... 80 9F-14 . . . . . . . . . . 81 8

31

F- IF,. . . . . . . . . .. 82 3

F-IllA . 15MI I.-D-81641 (AS) . .......... .84 R

Dest ination IndicatorS......... ...... . . . ... .5

-6-

NAMC--75267,-40

C 0 N T E N T 5 0 F r A HL , ( n t. ne d)

FUNCTI0N TABLE ENTRY FIGURE

Engine Torque DisplayCL-84 ... . . . . 86

Flap Status DisplayF-14 ....... 87

Flight Path Angle DisplayA-7 ........ . . ...... .. 88 26

33F-14 ...... . . . . . .. 89 26F-15 . . . . . ..... . . . 90 26AV-A . . . . .. ....... 91 27

Glide Slope Error DisplayF-14 . ........ . . . ..... . 92 31.F--14 .......... . . ...... 92 9F-111A .............. . . . . 93 ViCL-RA . ........ . . . . ...... 94

Ground Speed DisplerCL-84 ............ . . . . . 95AV-SA .......... . ..... . .. 96 54

Gun Aiming SybolA-7 .......... . . ..... . 97 ;5F-5 .......... . ....... .. 98 4F-14 ........ . ........ .. 99 to

36F-15 ..... ... . .. . .. 100 1AV-8A . ....... .. 101 37

Heading CowmandF-15 ........ . . ......... 102 36CL-84 ........... 103 1MIL-D-81641(AS) . . . . . .. 104 38MII-STD-884B . . . . . . . . . . . 105 38

Hezding DisplayA-7 .......... . ........ 106 39F--14 . . . . . . ...... 107 40

41F-15 .......... . ..... . .. 108 38CL-84 .......... . . ...... 109 1AV-8A .......... . . ...... 110 3qMIL-D-8164](AS) ...... . .. . ....... .. 111 38MIL-STD-884B ...... . . .... ...... 112 38

Impact Point Display-14 .. . .. . ..... . . 113 1

:[L, -7

NAC,.- 75267--40

C 1.) N V Ji N T N 0 V T1' A RI L 1! n t i it ei •t )

FUNCTION TABLE ENTRY FIGURE

Impact Point Display (Continued)AV-8A ............ . . .... 114 42MIL-D-81641(AS) .. .... .. . . ...... 115 10

35

Mach Number CommandF-14 .. ........ . . ....... 116 3All-8A ............ . .. ... 117 6MIL-D-81641(AS) ... ..... ... ... 118 5

Mach Nui.ber DisplayF-14 .... . . . . ......... 119 3F-. . . . . .. . 120AV-8A ........ . . ...... . 121]MIL-D-*81u41(AS) ........ . . ..... .. .. 122 5

Master Arm Status IndicatorF-14 ... .123

F-15. ........ . . ...... .. 124 22MII,- 21641 (AS) . .......... . . .. .. 125

Missile Target DisplayI 41.--81641 (AS). ..... . ......... 126 35

Missile Target Status IndicatorMIL-D-,81641 (AS).127 43

Navigation Advisories DisplayF-15 .. . . .... . 128

Navigation Mode Selection IndicatorF-.15 .. ....... ... . 129

Pitch Error Display,F--111A . ...... 130 15

Range to Destination DisplayF-15. 1 1....... .131,

Range--lo-(Go to In-Range bi)l 5playF-... .32 1.3 .-

Range--Tn.(o to lPuilup Point DiisplayA..7 .. 133 13F-- 14 ... . .. . U54 13F1-.Is ................ . .... 135 44MI,.LI)--81641 (AS).... ... . • .. 136 45MIIL-Srl8841 . . . 137 45

NADC-75267-40

CONTENTS OF TABLES (cun tinued)

FUNCTION TABLE ENTRY FIGURE

Rang3-To-Go to Weapon Release DiaplayA7o. . . . 138 13

A-7..................... ....... * 183

F-14 . . . .. . ...... 139 1

F-IS ............... 140

MIL-D-81641(AS) . .. . . . . ..... 141 45

MIL-STD-884B .................. .. 142 45

Rotation Angle CommandMIL-D-.81641(AS) . . . . ... . . .. 143 23

Runway Image DisplayCL-84 .......... . ....... . 144 1

MIL-D-81641(AS) ............ 145 46

MIL-STD-8843 . ......... 146 47

Sensor Scan DisplayF-14 .......... . . ....... 147 48

8

F-15 ........ . . ......... 148 12

AV-8A ...... . .......... . . 149

Sight-Line Depression Angle DisplayAV-SA .... . . ......... 150

Speed Error Display (IAS)F-1lIA . . . . . . . . . . .

AV-8A ............ . . ...... * 1'2 6

Standby ReticleA-7 .. . . .......... 153 51

P- 4. . . . . . . . . . . '154 52F-14 .. .

MY L-D-81641(AS) . . . . . ... . . 155 53

Tacan Deviation Displa)F-14 .......... . . ..... . 156 24

AV8 . . 157 59AV-BA............................173

Target in Range IndicationA-7 .......... . . ........ 158 35

13

F-is ...... . ...... 159 56

MIL-D-81641(AS) ............ . . .... 160 43

Target Out of Range IndicationF-14 .......... . . ....... 161 8

Target Range DisplayF.- 5 .. . . .............. 162

9

NADC-75267-40

C 0 N T r; V T 0i; 0 1 T A B LE S (c o n ti n u e d)

FUNCTION TABLE ENTRY FIGURE

Target Rai4ge Display (Continued)F-14 .......... . .......... 163 54

5536

F-IS . ........ . . .......... 164 56MTL-D-81641(AS). ......... . .......... 165 57

Terrain Contour DisplayMIL-D-81641(AS) ...... . ......... 166 58MIL-STD-884B .... . . ...... . 167 58

Time-To-Go to Weapon Release DisplayF-14 .......... . ......... 168 10F-111A .......... . . . . .... 169 15

SUHF Homer DisplayAV-8A ........ . . ......... 170 39

Velocity Vector DisplayA-7 ............ . . .... 171 9F-14 . . . . . . . . . 172 9F-iS .......... . . .... .. 173 9MIL-D-81641(AS) .......... . ........ . 174 45MIL-STD-884B . . . . .. . .......... 175 45

Vertical Speed CommandMIL-D-81641CAS) ...... . .. . ...... ... 176 SMIL-STD-884B .......... . .......... 177 5

Vertical Speed DisplayA-7 ........ . . . . ...... 178 2F-14 . . . . . . . . . . . 179

CL-84 . . . ........... 180 1AV-8A . ................... 181 19MIL-D-8164J!'AS) . ..... . . . . . .... 182 5MIL-STI)-8B4. .. . .... . . . ... .. .. 183 5

Visual Search Area DisplayF-15 .. . . . .. . ...... ... 184 59F-IIIA .......... . ......... 185 15

Warning Signal IndicatorA-7 .......... . .......... 186 60F-14 .......... . .......... 187 61F-1s .......... ........... 188MII.-ID-81641 (AS) .......... . .......... 189 61MIL-STP-884B .......... . .......... 190 61

10

NADC-75267-40

C O N T E N T S O F T A B LE S (c o n in i ed)

FUNCTION TABLE ENTRY FIGURE

Weapon Release Indicator

NIL-D-S1641(AS) . ........ 191 45

Win& Incidence DisplayCL-84 .............. 192 1

wing Sweep DisplayF-14 .......... .......... 191

'I

.1 - It11 ,

NADC-75267-40

IA

.4S 0

-~4 4-4 0

9: V

v u .

"U(I 9 o o o-1.4 A gj

- - C

412

NADC-7S267-40

Id

~~44a

-1 -

?4ADC-75267-40

40e

Af i

t4.~ 04 w I'It- - - - -

14S

NADC-7326--40 I,

_ I, ,11 *

i -

a lla

p- - - -.

"\4,

NADC-75267-40

'I I

I ~I

I I

24M 1?4 a O 140 0

.z 13

re. n

- 14 I n u q ~ t

Y2. 5, - r .

!16

14AD-75267-40

Al AS I-

10 C

W IIInI

.4 .U

01 0 . 14

N; s

*4 :5.. 1

4'. . '4 .4 4 .-

tP 04 O M

w A

.. , i. 3

z .2cwo.

K- Id

17

NADC-75267-40

49 A

F4.j I,

-C

20.0 Ai 6o .M

0 U 0

LM VO- WA

MIM

*.44

~It~i ~___ ______

'or

46 w __ ____

NAD-75267-40

Iw

-we 610 -

40 u

OUU

144 4 Id A -4 aI a z

La. x

* L9

N -19-

NADC-75267-40

fl u

40

SII 4

0 .4 4' l

-4 3

4 -4 ML .

4A

d9 ld4 I- 'II

U3. 0 --

200

NADC- 75267-40

pa a

di

4 .0

I" a

.4 . . .

144

I '

U . 4 0

A 31 x 4

WPM~

NADC,- 75267-40

%.4

U -4

P4~

Ali 4

.4 %A, Ol 4

E~i II ora

-. 44 4-.

1-

1- . 0 41 4

1 4 -, Of4n " 0 IA a 0 0

4; W 44 %= -, t Vi 0 01

44 A l

4411~ 0.4 4 4

z 0

tA *.4 i W

-. 22

HADC-75267-40

Ama.4

rmq

U lu.- : 140A4 U.

a N .OI~I0 1 4IU4wq a V-b14 o0*E C VaI sa

a a0

6 t 5

14-rx, at

23

NADC.-75267-40

0 44 14

.1~~. soi.ia v,4-4 ai*f. C -C 4.4

e u

.P4

I.. C4 0 t c t

a.'.

.4 4

.9 1414

94 4 U4 0 .

4c-4j.49

14V

Co

n -0:..cA 01

"4.j w

z- 4- W9

r4 -t

24 I

14ADC-7S267-40

ILI

0I a.

.3 W4

-. 4 a8

ac 61 AIn '4j 0

of 0 IQ

*-14 U4 to

9 S-4 C 0 -

04 A. -11

V~4 68 '. A

.0Il i .;I 8

Li14K 68 Lw8 4488 M 66

U) 1 sec .0 '*0u u

lo.

D3 ~ .6

'4 ~ ~ ~ ~ ~ l a e A . g ~ .. U.S4-

64 1.4 .'010

-25-

NW-C75267-40

dia

U .4M.4

a, b: UL a

.034

.4-

"262

MM-C75267-40

11

u27U - ,.1

' -" •ii

SI I

-4 .. ..

5 1

i ,'.4

Si~

- 27 -

NADC-75267-M

II

I -K

N *4

fa2rg ;a

MADC-75267-40

'ao

* .4.I4

0 ~ 0

44 N

aa

!9 -.4 344 ~41

et 00

"41l ei4*

____ v_ _ _ _ _ _ 1429 -a

MAM-15267-40 2

.1 a

cAl

.4 00I

-. 44

V. .4

.5.

.~ as

r40 0

'"4 1-4.

-1 14449 14 1A

9L 1 "a -

14--4

14V

U8 13 6

'-44

In !n to 'I U

0 .4

t-4

PC.

30.

N/ADC-75267-40

t E Ij'

b '

i . A:

in d ,

"" a 1 ,

" • i "' <"- ...... 'r:" .. . .......... " .. .. ........ • ""i" .... ll..... ...... .... |"• .. . : .... " "--• ••' . :•...

KAflC-75267-40

V N4

all.

110 11-uA .0 0.4 0 C0.

YD . 0 40

u 45 0 4.~ ~ U4 aU

0 *

rl 0

144

AlU -

CI 4 ) 4

'P4

?4ADC- 75267-40

-,

*4@4MInI

In.

3.4 4, A

m 33

MADC- 75267-40

-P4

~ 414

aa

OL ft ~14

I'i

-44

IN vsti Ij

-434

NADC-7S267-40

64 14

044

A 4

a ul aL

w *- 1-4

4 . tn n. nSU U 4

Mw 0

N~ADC-75267- 4 0

40 I

b4 to '-0-

14 .01

*4 U 0 0 6) '4 c

-- el .it +-) D.. _ _ _ _ _ _ w

t1

NW'4

e u

C) 0 6)1el

tn 13

36

MADC-75267-40

0 4.

00 0 aI

14.

SI *0

(0 v

lo 0

Z ~14

cc 0 '4 41. 0 1

14 1-4 Ch 0 41 a ., 04 0 b 0 0 0gn 'r 4.4 r.I m N~ >. ... u .4 9

V .

u-I~~ 4. S A'.4W4

04 -

Cc~ ~ 0. 1AS' 0 . 4 1

-~ ~~~~~ =4 @6 0~ I 0 ~ 0 ' I . 0~to I 0 C ~ V a Eý ~. N..

N t' CA-

I4 SI4 w Ul

-W

NAD -754267-40

*13I

'.2.

Ito- 14- 5

94

4P

U, iz

N~38

NADC-75267-40

44

to 60a

1114

-C4

F V

II

-44

'.I I I-n! j - !

g~~4 ~ ____

Si,4,

NADC-75267-40

SAi .

U W

lmm

94)a;n

* 4 *• " •'-

n z

R K I

40~

S M .

NADC-7S267-40

a a 4

M 4

1*41

NADC-75267-,40-.. p

I

. III- - - I-------

3in

.U2

42.

*,1 t 1 * I , "

SIE ! i :

St U , dI

j. 0 ,

SI,.3

I.'"' '. t

;.•.4 U A "' V

- 42

NADC-75267-40

An b. 00

"",ii~ I U I I,

Ii+ i,. 111

0 ta

- - w - -- - - 4- --.

-43-

NADC-7S267-40

S I I _ _ I I___ _

145

in ILP. ar a

~444

- i n

U4r

U 43

It !,_ _ _

4,5

- N - 4s 1-_

pW4

4.14

* 144

WP *

ILIA

tnv

51-4

0x

-46

NADC- 75267-40

16

U4

r4 _F5ii

474

NADC-75267-40

* Ihil~*i I IM~

Op~. 0 .a0 aC

0 0 14 0 t &

44

*JtE.:

A~ r4

in. f. I

1: 1-

48

NADC-75T67-40

I S 4

* t

i 6I *11.~~

i 5 4A I ;,.

= I ,-,!

II

AP-

-49-

NADC-75267-40

ý4f

--

fil

I : ' D

".4e

n InU4 .0

o It"

€GD

ii

ILII

U UP

-4-

1"1ID ~

- 50 -

i• I I I I I I I I I I I

I'

I>

NMJc�.. 7526 7-4�

/LIU U I

I.u &

b4 U

1.4 EU0

U*g U,-

'

8

-4

� �j

-4

ii

LI0 U

144

8

I- U)

'I,

A'

NWD-75267-40

84

00

14 4'-

a0 sno 0

0'0

tAA

H lln4

C.

tl V

NA'X-75267-40

VA

lie

-et -

-s'

II cq ý-1

9 5~I S 53

NAD(>.752ýi7-4O

I. w

V4 -4 Iwo_ _

.4~

c 26

44 06.441

an~

W - N 4j4, 1. U

ri 0 a~ .4 04 -

ODO

4,4

$43 U %dC3

a 0 U

544

NAi)C-75267-40

.50

441

- ~ ic ii

-55

NADC-75267-40

SO -

%,.

7o

56

- 56 -

NADC-75267-40

A

100~

0) .

IO

ASA- 5L -,

-57/

NAIC.75267-40

soFLIGH4T DIRECTRo

/ ' FIXEDRETICLE

VELOCITY VECTORMOVEABLERETICLE

.. Fig. 9 Fill. 10

Fi. It Pri. 12

-, 58 j

NADC-75267-40

Fig. 13 fti. 14

34-

Fig. 15 Fil. 16

- 59 -

NADC-75267-40

3000

2:10

>0

®~CR

06

II

NADC-IS267-40

Or-A

l1g. 21 F1S. 22

10

nr

FIt. •r ig. 24

NADC-75267-40

-0 r w!

rigt. 2s Fit. 26

it.6

Figl. 27 IFIio 26

S 62. -

NADC-75267-40

0 o7,,

2~

?ix. 19 Fir'. 3-:

VELOCITYVECTOR

FLIGHTDIRECTOR

-63.-

NADC-75267-40

-- 5 -

I,.

I,.

Fir '. 57 .

64

NADC-75267-40

11 12 13

is 19 20 32 3

65

NADC- 75267-40

10 11 12' a I

A-

(130

"Ftr,, 4,1 P•ig. 4,4

66 o.

NADC- 75267-40

-ate . j

00

67--- 67J

NADC- 75267-40

1, 4'.---.

rig. 51 F ig. 52

68

NAIDC-75267*-40

// .20

40-

100

-La. Pi't. 54

-. 69-

94ADC-75267-40

0 1 2 3 4 6

S57 7 5,1

L7

• II il I I.../1 I 7/7/Ii

NADC-75 26 7-40

-71-

NADC-75267-40

MO D E S

A-7 F-111A

En Route Navigation Manual,Terrain following CommandLanding DiveData Link Long Angle Drogue Delivery

Norml Attack Bomb HomingNormal Attack Offset Bomb Guns/RocketsRadar Bomb , L

Radar Bomb Offset Bomb CL-84Navigation Bomb AGun Approach - "

Rocket Transition

F-S AV-A 8A

Guns Before AFC 105:Missile V/STULManual GEN

NavigationF-14 REV

Takeoff/Manual A/A

Takeoff/TACAN After AFC 105:Cruise/Vector V/STOLCruise/TACAN NavigationCruise/Manual Weapons aCruise/Destination Weapons bA/A Manual Gun A/AA/A Optical TrackA/A Sidewiinder Boresight MIL-D-81641(AS)A/A Sidewinder NurmalA/A Phoenix Boresight Takeoff/NavigationA/A Phoenix Normal Terrain FollowingA/A Sparrow Boresight BombingA/A Sparrow Normal Boresight WeaponsA/G Computer-Initial Point Guided WeaponsA/G Computer-Target LandingA/G Precision Course Direction Boresight

A/G Computer-Pilot (Bomb) StandbyA/C Computer-Pilot (Guns, Rockets)A/G Manual MIL-STD-884BLanding/VectorLanding/All Weather Laiving TakeoffLanding/TACAN Navigation

Terrain Following/Terrain AvoidanceF-15 Weapon Delivery

Attitude Director Indicatoe Landing

A/A (Gun)A/A (Missile)A/C

-72-

-,_Iw &

NADC-75267-40

LIST OF ABRREVIATIONS

A/A Mir-To-Air

A/C Aircraft

ADI Attitude Director Indicator

ADL Armament Datum Line

AFC Airframe Change

"A, AMr-To-Ground

AILA Automatic Instrument Landing Ar-roach

ALT Altitude

AOA Angle of Attack

APPR Approach

ASH Allowable Steering Error

AWL All-Weather Landing

BARO Barometric

CCIP Continuously Computed Impact Point

CL Centerline

COMP Computer

DIV Dive

FD Flight Director

FOV Field of View

PPM Flight Path Marker

FRL Fuselage Reference Line

HOR Horizontal

IAS Indicated Airspeed

ILS Instrument Landing System

INS Inertial Navigation System

IP Initial Point

- 73 -

NAMJ-75267-40

L t , T OF AflBREVIATIONS (continued)

KT Knot

LADD Long Angle Drogue Delivery

LDG Landing

1 Mach

NAV Navigation

NM Nautical Mile

PCD Precision Course Direction

RNG Range

SEAM Sidewinder Expanded Acquisition Mode

SPEC Specification

SYM Symbolic

TA Terrain Avoidance

TAS True Airspeed

TCN TACAN

TF Terrain Following

TGT Target

TIERlO Thermometer

TO Takeoff

TRAN Transition

V/STOL Vertical/Short Takeoff and Landing

VV Velocity Vector

WPN(S) Weapon(s)

-174

NADC-75267-40

REFERENCES

1. HATOPS Flight Manual A-7E Aircraft; I4AVAIR 01-45AAE-I; changed 15 Aug1971.

2. F-S Technical Orders; T. 0. IF-SE-1.3. Preliminary HATOPS Flight Manual F-14A; NAVAIR 01-F14AAA-1; 1 Nov 1973.

4. F-14A Programmable Display Generator HUD Symbology/Interface Requirements;Grumman Aerospace Corp Report No. ASI-232-R-73-7; 22 Oct 1973.

5. F-IS (untitled)6. F-IS Product Support Digest; Ready Room pp 8-12.7. F-IlIA Technical Orders; T. 0. IF-Ill(V)A-1.S. Gold, T. and Walchli, R. M.; Head-Up Display for All-Weather Approach and

Landing of Tilt-Wing V/STOL Aircraft; AIMA Paper No. 74-952; 12 Aug 1974.9. NATOPS Flight Manual AV-SA; NAVAIR 01-AVOA-1; changed 15 Feb 1974.10. MIL-D-81641(AS); Display, Head-Up, General Specification for; 26 Jun 1972.11. NIL-SIT-884B; Military Standard Electronically or Optically Generated Dis-

plays for Aircraft Control and Combat; Cue Information; 4 Jan 1972.

t5

top related