Radar System Engineering

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306 ANTENNAS, SCANNERS, AND STABILIZATION [SEC.9.17 servoamplifier, and the follow-up system which includes the servomotor, the gear train or linkage system, and a take-off actuated by the controlled member. The gyro may be mounted on the rotating scanner or remote from the scanner, using slip rings and resolvers to take off the required error information. The error is fed into a servoamplifier whose output operates the servomotor which in turn aligns the antenna with the horizontal through a gear train or linkage system. The gyro should preferably have either a two-speed erection mechanism or a device to disconnect the erection mechanism when the aircraft goes into a turn. In a turn the gyro rotor tends to align itself with the resultant of the true gravity and the centrifugal force caused by the acceleration in the turn, instead of with true gravity alone. This can be minimized or eliminated by using a two-speed erection mechanism, or by employing an electromagnetic clutch to throw out the erection system entirely in turns. Continuing the general classification previously referred to, stabilizers may be further typed as stable-base, roll, or line-of-sight, depending on the stabilization compensation afforded. The stable-base stabilizer, as the name indicates, provides complete stabilization of the platform upon which the antenna is mounted. This requires use of a two-axis gyro transmitter to provide alignment or error information for both roll and pitch axes. The gyro is usually mounted remotely from the antenna structure in this type. In addition two separate servoamplifiers and follow-up channels are required, one for the roll-error component and one for the pitch-error component. Although this provides complete stabilization, the weight of the components usually appears excessive so that another type is preferable. The roll stabilization referred to is stable-base stabilization with the pitch channel removed. This requires a single-axis gyro transmitter for the roll axis, and but one servoamplifier and follow-up channel. Roll stabilization would be appropriate in large aircraft for which the pitch component might be negligible or tolerable. In deciding between a roll and a platform stabilizer the accuracy requirements must be balanced against the weight added by the pitch channel. The line-oj-sight method is one which maintains the axis of the beam of radiation in a horizontal position or a fixed angular distance above or below the horizon as the antenna rotates, scanning the horizon. This is done by automatically tilting the antenna about an axis perpendicular to the plane of the beam and parallel to the floor of the aircraft. Figure 9.35 shows the stabilizing attachment, A>-/.~\.15,5, mounted for photographic test on the scanner of the A>”/.iPS-2 circular-scanning radar. The black tubular construction of the scanner yoke can be seen, together with the silver-plated +in. coaxial transmission line. The 29-in. paraboloid has
SEC. 9.17] STABILIZATION OF’ THE BEAM 307 been removed from the gently curved support casting, which can be seen supported bet\veen the tilt bearings at the tips of the yoke. A table clamped to the yoke supports the gyro-torque unit and a servoamplifier. The gyro is mounted in gimbals and is provided with one synchro take-off FIG. 935,-A stabilizing attachment mountwl on an airbornescanner. The reflector has been replaced by a camerafor test purposes. at the gimbal axis parallel to the tilt axis. A synchro is also located at the output crankshaft of the torque unit. The servoamplifier essentially amplifies the algebraic difference between the voltages from these takeoffs, and thus actuates the motor in the torque unit to assure alignment between the output shaft and the gyro. The output shaft is linked to the paraboloid support by a rod seen at the bottom of Fig. 035. When there
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CHAPTER 1 INTRODUCTION BY LOUIS N.
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4 IN TRODUC7”ION [SEC.1.2 flik~c
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6 INTRODUCTION [SEC.1.3 pulse leaki
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8 INTRODUCTION [SEC.1.4 antenna is
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10 INTRODUCTION [SEC.14 step in out
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12 INTRODUCTION [SEC.1.5 where high
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14 INTRODUCTION [SEC.1.6 England, F
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16 INTRODUCTION [SEC.1°7 Microwave
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CHAPTER 2 THE lU.DAR EQUATION BY E.
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20 THE RADAR EQUATION [SEC.22 radia
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22 THE RADAR EQUATION [SEC.25 Again
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24 THE RADAR EQUATION [SEC.2.5 time
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26 THE RADAR EQUATION [SEC.2.5 smal
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28 THE RADAR EQUATION [SEC.!2.7 lim
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30 THE RADAR EQUATION [SEC.28 Anoth
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32 THE RADAR EQUATION [SEC.28 first
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34 TIIE RADAR EQUATION [Sm. 29 the
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36 THE RADAR EQUATION [SEC.2.10 (Vo
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38 THE RADAR EQUATION [SEC.210 prac
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40 THE RADAR EQUATION [SEC.2.10 tai
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42 THE RADAR EQUATION [SEC.2.11 swe
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44 THE RADAR EQUATION [SEC.2.11 res
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46 THE RADAR EQUATION [SEC.211 Alth
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48 THE RADAR EQUATION [SEC.212 othe
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50 THE RADAR EQUATION [SEC.212 The
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52 THE RADAR EQUATION [SEC. 2.12 Th
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54 THE RADAR EQUATION [SEC.213 smal
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56 THE RADAR EQUATION [SEC. 2.14 an
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58 THE RADAR EQUATION [SEC.2.15 not
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60 TIIE RADAR EQUATION [SEC.2.15 wt
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62 THE RADAR EQUATION [SEC.215 per
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64 PROPERTIES OF RADAR TARGETS [SEC
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66 PROPERTIES OF RADAR TARGET,S [SE
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PROPERTIES OF RADAR TARGETS [SEC.37
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88 PROPERTIES OF R.41~.l R T.-lRGE~
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92 PROPERTIES OF RA1l.4R TARGETS [S
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SEC.315] STRUCTURES 99 example, the
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SF,C. 3.16] CITIES 101 reflection w
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SEC. 3.16] CITIES 103 signal repres
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SEC. 3.16] CITIES 105 four signals
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108 PROPERTIES OF RADAR TARGETS [SE
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112 PROPERTIES OF RADAR TARGETS [SE
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CHAPTER 4 LIMITATIONS OF PULSE RADA
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118 LIMITATIONS OF PULSE RADAR [SEC
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122 LIMITATIONS OF PC’LSE RADAR [
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Page 128 and 129:
128 C-W RADAR SYSTEMS [SEC. 5.1 tar
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130 C-W RADAR SYSTEMS [sm. 53 point
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132 C-W RADAR S’YSTEMS [SEC.56 bi
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134 C-W RADAR SYSTEMS [SEC. 56 tran
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136 C-W RADAR SYSTEMS [SEC. 5.6 int
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138 C-W RADAR SYSTEMS [SEC, 5.6 rel
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140 C-W RADAR SYSTEMS [SEC 37 and j
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142 C-II’ RADAR SYSTEMS [SEC. 57
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144 C-W RADAR SYSTE.JfS [SEC. 58 gi
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146 C-W RADAR SYSTEMS [SEC. 58 Modu
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148 C-T RA DAR S YSTE.lf S [SEC. 59
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150 C-W RADAR SYSTEMS [SEC. 5.11 cy
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152 C-W RADAR SYSTEMS [SEC.5.11 Now
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154 C-W RADAR SYSTEMS [SEC.5.11 exc
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156 C-W RADAR SYSTEMS [SEC. 5.11 in
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158 C-W RADAR SYSTEMS [SEC. 5.12 Pu
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CHAPTER 6 THE GATHERING AND PRESENT
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162 THE GATHERING AND PRESENTATION
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168 THE GATHERING AND pRESENTA TION
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~70 THE GATHERING AND PRESENTA TION
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SEC. 66] PLANE DISPLAYS INVOLVING E
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SEC. 69] IiARLY AIRCRAFT-WARNING RA
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SEC. 69] EARLY AIRCRAFT-WARNING RAD
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f$Ec. 69] EARLY AIRCRAFT-WARNING RA
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SEC. 6.9] EARLY AIRCRAFT-WARNING RA
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SEC. 6.10] PPI RADAR FOR SEARCH, CO
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SEC. 6.11] HEIGHT-FINDING INVOLVING
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SEC.6.12] HEIGHT-FINDING WITH A FRE
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- - -— . .. —-— - .. —-.
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SEC. 612] HEIGHT-FINDING J~ITH A FR
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SEC. 6.13] HOMING 197 ber of the pa
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SEC.6.13] HOMING 199 usually made t
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SEC. 6.13] HOMING 201 application,
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SEC. 6.14] PRECISION TRACKING OF A
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SEC.6.14] PRECISION TRACKING OF A S
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SEC. 614] PRECISION TRACKING OF A S
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f$Ec. 614] PRECISION TRACKING OF A
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SEC. 615] PRECISION TRACKING DURING
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CHAPTER 7 THE EMPLOYMENT OF RADAR D
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SEC.72] AIDS TO INDIVIDUAL NAVIGATI
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SEC. 7.2] AIDS TO INDIVIDUAL NAVIGA
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SEC. 73] AIDS TO PLOTTING AND CONTR
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SEC.7.3] AIDS TO PLOTTING AND CONTR
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SEC.7.3] AIDS TO PLOTTING AND CONTR
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SEC. 7.4] THE RELAY OF RADAR DISPLA
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SEC. 7.51 RA DAR IN THE RAF FIGHTER
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SEC. 7.6] THE U.S. TACTICAL AIR COM
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SEC.7.6] THE U.S. TACTICAL AIR COMM
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238 THE EMPLOYMENT OF RA DAR DATA [
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240 THE EMPLOYiWENT OF RADAR DATA [
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242 THE EMPLOYMENT OF RADAR DATA [S
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244 RADAR BEACONS [SEC. 8 duration
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246 RADAR BEACONS [SEC. 8.1 beacons
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248 RADAR BEACONS [SEC.8.1 4. Porta
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250 RADAR BEACONS [SEC.8.2 Table 8.
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252 RADAR BEACONS [SEC.84 restricte
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254 RADAR BEACONS [SEC. 85 radar se
Page 256 and 257: 256 RADAR BEACONS [SEC.85 In the ca
Page 258: 258 It Al)AIt BEACONS [S,,c, S3 Sim
Page 261 and 262: SEC. 86] FREQUENCY CONSIDERATIONS 2
Page 263 and 264: SEC. 87] INTERR~A TION CODES 263 wi
Page 265 and 266: SEC. 8.9] TRAFFIC CAPACITY 265 diff
Page 267 and 268: SEC.8.9] TRAFFIC CAPACITY 267 which
Page 270 and 271: 270 RADAR BEACONS [SEC. 810 range a
Page 272 and 273: 272 ANTENNAS, SCANNERS, A.VD STABIL
Page 274 and 275: 274 ANTENNAS, SCANNERS, AND ST ABIL
Page 276 and 277: 276 ANTENNAS, SCANNERS, AND STABILI
Page 288: 288 ANTENNAS, SCANNERS, AND STABILI
Page 291 and 292: SEC. 913] THE AN/APQ-7 (EAGLE) SCAN
Page 293 and 294: SEC.913] THE AN/APQ-7 (EAGLE) SCANN
Page 295 and 296: SEC. 9.14] SCHWA RZSCHILD ANTENNA 2
Page 297 and 298: SEC. 9.14] SCH WA RZSCHILD ANTENNA
Page 299 and 300: SEC. 9.15] SCI HEIGHT FINDER 299 de
Page 301 and 302: SEC.9.15] SCI HEIGHT FINDER 301 In
Page 303 and 304: SEC.916] OTHER TYPES OF ELECTRICAL
Page 305: SEC,9.17] STABILIZATION OF THE BEAM
Page 309 and 310: SEC. 9.17] STABILIZATION OF THE BEA
Page 311 and 312: t$Ec. 9,18] DATA STABILIZATION 311
Page 313 and 314: SEC. 920] INSTALLATION OF SURFACE-B
Page 315 and 316: SEC. 922] STREA MLIA”ING 315 func
Page 317 and 318: SEC. 9.25] EXAMPLES OF RADOMES 317
Page 319 and 320: SEC.9.25] EXAMPLES OF RADOMES 319 a
Page 321 and 322: SEC. 10.1] CONSTRUCTION 321 of the
Page 323 and 324: SEC. 10.1] CONSTRUCTION 323 later r
Page 325 and 326: SEC.10.2] THE RESONANT SYSTEM 325 m
Page 327 and 328: SEC. 1021 THE RESONANT SYSTEM 327
Page 329 and 330: SEC. 10.2] THE RESONANT SYSTEM 329
Page 331 and 332: SEC. 103] ELECTRON ORBITS AIVD THE
Page 333 and 334: SEC. 103] ELECTRON ORBITS AND THE S
Page 335 and 336: SEC. 103] ELECTRON ORBITS AND THE S
Page 337 and 338: SEC. 10.4] PERFORMANCE CHARTS AND R
Page 339 and 340: SEC. 10.4] PEIWORMilNCE CHARTS AND
Page 341 and 342: SEC. 10.5] MAGNETRON CHARACTERISTIC
Page 343 and 344: SEC.105] MAGNETRON CHARACTERISTICS
Page 345 and 346: SEC. 105] MAGNETRON CHARACTERISTICS
Page 351 and 352: SEC. 10.5] MAGNETRON CHARACTERISTIC
Page 353 and 354: SEC. 10.6] MAQNETRON CHARACTERISTIC
Page 355 and 356: L%C. 10.6] MAGNETRON CHARACTERISTIC
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SEC. 10.7] PULSER CIRCUITS 357 and
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SEC. 10.7] PULSER CIRCUITS 359 tude
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SEC. 10.7] PULSER CIRCUITS 361 cen~
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SEC. 108] LOAD REQUIREMENTS 363 TAB
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SEC. 10.8] LOAD REQUIREMENTS 365 to
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SEC. 109] THE HARD-TUBE P ULSEh? 36
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SEC. 10.9] THE HARD-TUBE P ULSER 36
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SEC 10.9] THE HARD-lUBE PULSER 371
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Sl?lc.10.91 LINE-TYPE PULSERS 373 D
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SEC. 10,10] LINE-TYPE PULSERS 375 i
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SEC. 10.10] LINE-TYPE PULSERS 377 I
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SEC. 10.10] LINE-T YPE PULSERS 379
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SEC. 10.10] LINE-TYPE PULSERS 381 T
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SEC.10.11] MISCELLANEOUS COMPONENTS
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SEC. 1011] MISCELLANEOUS COMPONENTS
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R-F CHAPTER 11 COMPONENTS BY A. E.
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SEC.11.2] COAXIAL LINES 393 Why a M
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SEC.11.2] COAXIAL LINES 395 lines h
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SEC.11.2] COAXIAL LINES 397 since n
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SEC,113] JVA VEGUIDE 399 than a qua
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i?EC. 11.3] WA VEGUIDE 401 too grad
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SEC. 113) WA VEGUIDE 403 types of m
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SEC. 11.4] RESONANT CAVITIES 405 co
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SEC. 11.5] D,C”PLEXING AND TR SWI
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SEC. 115] DUPLEXING AND TR SWITCHES
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SEC. 11.5] DUPLEXING AND TR SWITCHE
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SEC.11.6] THE MIXER CRYSTAL 413 sem
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SEC. 11.7] THE LOCAL OSCILLATOR 415
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SEC. 11 .8] THE MIXER 417 minimum l
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SEC.11.10] REASONS FOR AN R-F PACKA
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SEC. 11.11] DESIGN CONSZDERA TZONS
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SEC.11.11] DESIGN CONSIDERATIONS FO
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SEC. 11.12] ILLUSTRATIVE EXAMPLES O
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SEC. 11°12] ILL US’TRA TIVE EXAM
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SEC. 11.12] ILL USTRA TIVE EXAMPLES
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SEC.11.12] ILL US1’IiA TI VE EXA
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CHAPTER 12 THE RECEIVING SYSTEM—R
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SEC. 122] A TYPICAL RECEIVING SYSTE
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SEC.12.2] A TYPICAL RECEIVING SYSTE
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SEC. 122] A TYPICAL RECEIVING SYSTE
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SEC.12.3] SPECIAL PROBLEMS IN RADAR
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SEC.12.4] I-F AMPLIFIER DESIGN 443
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SEC.12.4] I-F AMPLIFIER DESIGN 445
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SEC.124] I-F AMPLIFIER DESIGN 447 i
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SEC. 125] SECOND DETECTOR 449 This
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SEC.12.6] VIDEO AMPLIFIERS 451 ampl
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SEC.12.7] A UTOMA TIC FREQUENCY CON
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SEC. 12.7] A UTOMA TIC FREQUENCY CO
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S~C. 128] PROTECTION AGAINST EXTRAN
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SEC. 128] PROTECTION AGAINST EXTRAN
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SEC. 12.8] PROTECTION AGAINST E-YTR
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&- L,-self resonant COIIS at mterme
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J All resistors~ watt Interstate co
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SEC. 12.10] LIGHTH”EIGIIT AIRBOR.
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s, 0.001 $180 b To reflector To sea
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+ 180v T +120V 470 470 470 470 e“
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SEC.12.11] AN EXTREMELY WIDEBAND RE
Page 475 and 476:
CHAPTER 13 THE RECEIVING SYSTEM—I
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SEC.13.1] ELECTRICAL PROPERTIES OF
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SEC 13.2] CATHODE-RAY TUBE SCREENS
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SEC.13.2] CATHODE-RAY TUBE SCREENS
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SEC. 13.3] SELECTIO.V OF THE CATHOD
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SEC. 13.3] SELECTION OF THE CATHODE
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SEC. 13.4] ANGLE-DATA TRANSMITTERS
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SEC.13.4] ANGLE-DATA TRANSMITTERS 4
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SEC. 13.5] ELECTROMECHANICAL REPEAT
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SEC. 13.6] AMPLIFIERS 493 whence th
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SEC. 13.6] AMPLIFIERS 495 by using
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SEC. 13.7] GENERA TION OF RECTANGUL
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SEC. 13.7] GENERATION OF RECTANGULA
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. SEC. 13.8] GENERA TION OF SHARP P
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SEC. 139] ELECTRONIC SWITCHES 503 T
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SEC. 13.9] ELECTRONIC SWITCHES 505
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SEC. 13.9] ELECTRO.VIC ISWI TCHES 5
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SEC. 13.9] ELECTRONIC SWITCHES 509
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SEC. 1310] SAWTOOTH GENERATORS 511
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SEC.13.10] SAWTOOTH GE,VBliATOh?S 5
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SEC. 1311] ANGLE INDICES 515 bright
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SEC. 13.11] ANGLE INDICES 517 the s
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. . “4 100k.lw $4.7k-lw .& t, T 0
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SEC.K3.121 RANGE AND HEIGIiT INDICE
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i%C.13121 RANGE AND HEIGHT INDICES;
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SEC. 13.13] DESIGN OF A-SCOPES 525
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SEC. 1313] DESIGN OF A-SCOPES 527 f
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SEC.1314] B-SCOPE DESIGN 529 \
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SEC. 13.14] B-SCOPE DESIG.V 531 wil
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Trigger I I I (CT)Sawtooth —. (A)
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SEC.1316] RESOLVED TIME BASE PPI 53
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SEC. 13.16] RESOLVED mi? TIME BASE
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SEC. 13.17] RESOLVED-CURRENT PPI 53
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SEC. 13.17] RESOLVED-CURRENT PPI 54
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+ 200V— — — J 60k . Llk )k 60
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SEC. 13.19] 1’HE RANGB-ll EIGII1
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SEL!. 13.19] THE RANGE-HEIGHT INDIC
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SEC. 13.20] RESOLUTION AND CONTRAST
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SEC. 13.211 SPECIAL RECEIVING TECHN
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554 THE RECEIVING SYSTEM-INDICATORS
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556 PRIME POWER SUPPLIES FOR RADAR
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. . . 0.9 P~- 860-’CPS CF over 2
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Page 562 and 563:
562 PRIME POWER SLTPPLIES FOR RADAR
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Page 572:
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SEC. 14.6] SPEED REGULATORS 575 ‘
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SEC. 146] SPEED REGULATORS 577 havi
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SEC. 14.7] DYNAMOTORS 579 14.7. Dyn
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SEC.14.8] VIBRATOR POWER SUPPLIES 5
Page 583 and 584:
SEC. 1410] FIXED LOCATIONS 583 port
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SEC. 14.13] ULTRAPORTABLE UNITS 585
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SEC. l’k~~] SHIP RADAR SYSTEMS 58
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SEC. 151] INTRODCCTIO,\- 589 the pr
Page 591 and 592:
SEC, 152] NEED FOR SYSTEM TESTING 5
Page 593 and 594:
SEC, 153] INITIAL PLANNING AND OBJE
Page 595 and 596:
SEC. 15.4] THE RANGE EQUATION 595 n
Page 597 and 598:
SEC. 15.5] CHOICE OF PULSE LENGTH 5
Page 599 and 600:
SEC. 15.7] AZIMUTH SCAN RATE 599 to
Page 601 and 602:
SEC. 15.8] CHOICE OF BEAM SHAPE 601
Page 603 and 604:
SEC. 15.8] CHOICE OF BEAM SHAPE 603
Page 605 and 606:
SEC. 15.9] CHOICE OF WAVELENGTH 605
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SEC. 15.10] COMPONENTS DESIGN 607 1
Page 609 and 610:
SEC.16.11] MODIFICA TIO.VS A,YD ADD
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SEC. 15.12] DESIGN OBJECTIVES AND L
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SEC. 15.12] DESIGN OBJECTIVES AND L
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SEC. 15.13] GENERAL DESIGN OF THE A
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SEC. 15.14] DETAILED DESIGN OF THE
Page 619 and 620:
SEC. 15.14] DETAILED DESIGN OF THE
Page 621 and 622:
,/ / /“)4 Providenc~ (b) Fm. 16.1
Page 624 and 625:
624 EXAMPLES OF RADAR SYSTEM DESIGN
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CHAPTER 16 MOVING-TARGET INDICATION
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628 MOVING-TARGET INDICATION [SEC,
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630 MOVING-TARGET INDICATION [SEC.
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632 MOVING TARGET INDICATION [SEC.
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Page 646 and 647:
. 646 MOVING- TARGET INDICATION [SE
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648 MOVING- TARGET lNDICA TION [SEC
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652 MOVING-TARGET INDICATION [SEC 1
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656 MOVING-TARGET INDICATION [SEC.1
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658 When o = Othe instead MOVING-TA
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662 MOVING TARGET INDICATION [SEC.1
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670 MO VINGTARGET INDICATION [SEC.
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672 MOVING TARGET INDICATION [SEC.1
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674 MOVING- TARGET INDICATION [SEC.
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676 MOVING-TARGET INDICATION ~SEC.
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CHAPTER 17 RADAR RELAY BY L. J. HAW
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682 RADAR RELAY [SEC. 172 transmitt
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684 RADAR RELAY [SEC. 17.3 staggeri
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686 RADAR RELAY [SEC. 17.4 excluded
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688 RADAR RELAY [SEC. 174 long sign
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h Video I 1 I Angle marks RADAR REL
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692 [SEC. 175 ḇ 1 1 1 I ~ LKal tr
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694 RADAR RELAY [SEC. 17.5 generato
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696 RADAR RELAY [SEC. 17.6 station
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698 RADAR RELAY [SEC. 17.6 Video si
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700 RADAR RELAY [SEC. 176 train. Th
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702 RADAR RELAY [SEC.17.7 be obtain
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704 RADAR RELAY @EC. 17.7 illustrat
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[11 1 Bas,c pulse I %e pulse i ~--.
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708 RADAR ltELA Y [SEC. 1743 wave f
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710 RADAR RELAY [SEC. 17.8 actual m
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. 712 RADAR RELAY [SEC. 17.9 Such a
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714 RADAR RELAY [SEC. 17.10 between
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716 RADAR RELAY [SEC. 17.10 signal
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718 RADAR RELAY [SEC. 17.11 suppres
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720 RADAR RELAY [SEC. 17.12 provide
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722 RADAR RELAY [SEC. 17.13 relay l
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724 RADAR RELAY [SEC. 17.14 TaLE 17
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726 RADAR RELAY [SEC. 17.15 RADAR R
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728 RADAR RELAY [SEC. 17.15 Modulat
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730 RADAR RELAY [SEC. 17.15 the sec
Page 732 and 733:
732 RADAR RELAY [SEC. 17.10 pulses
Page 734 and 735:
734 RADAR RELAY [f+iEc.17.16 The vi
Page 737 and 738:
Index A Absorbent materials, 69 Abs
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INDEX 739 B-scope, electrostatic, 5
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INDEX 741 Fairbank, W. M.,80 F Fan
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INDEX ’743 Microwave, reason for
Page 745 and 746:
INDEX 745 Radar, pulse,3 range perf
Page 747 and 748:
INDEX 747 Signal, interference of,
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Radar System Engineering

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