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Bode diagrams, 307
equivalent derivative method, 304, 307
frequency response methods, 270, 304, 305
Linear Quadratic Gaussian (LQG), 317, 318
Linear Quadratic Optimization (LQ), 316, 317
Nyquist diagrams, 307
root locus methods, 270, 308–310
singular value methods, 321
time domain methods, 317, 317
stability boundaries, 137, 138, 267, 268
stability derivatives
aeroelastically corrected, 298
dimensional, 262, 266
nondimensional, 264–266
rotary, 266, 267
stability derivative extraction, 224–229
elementary methods, 224, 225
extended Kalman filter method, 226, 227
maximum likelihood method, 225, 226
unstable airframe, 227
weight moment method, 224
Stack, John, 162, 163, 166
stall recovery, 252, 253
Standard Atmosphere, 277, 278
Stanford University, 13, 19
Stapleford, Robert, 32, 309, 320
Staples, K. J., 17
state-variable formulation, 274, 276
state vector, 276
static margin, stability, 12, 30, 336
Statler, Irving C., xix, 128
stealth aerodynamic issues, 335–340
faceted airframes, 335–337
parallel-line planforms, 337, 338
suppressed or no vertical tails, 338–340
Stearman-Hammond Model Y, 233
Stearman, Ronald O., 218, 219
Steer, A. J., 322, 343
Stengel, Robert F., 16, 328, 355
inertial coupling analysis, 120
LQ stability augmenter design, 317
on LQG controllers, 317, 318
pilot cues, variable-stability airplanes, 38
single pilot IFR operations, 242
stability derivative extraction, 227
supersonic modes of motion, 182–184
Sternfield, Leonard, 67, 115, 181, 274, 275
Stephens, A. V., 121–123
Stephens, William C., 310
Stevens, B. L., 15
stick force levels, 57
stick force per g, 28
stick pushers and shakers, 178
Stinson Reliant SR-8E, 22, 24, 25
Stough, H. Paul III, 126, 134
Stout Sky Car, 233
Street, William G., 57–59
stretch, control cable, 24, 29, 127
Stinton, D., 18, 32
Strumpf, Albert, 284
Sud Caravelle, 173
Sukhoi Su-27, 157, 253
supermaneuverability, 157–161
control for recovery, 157, 161
Cobra maneuver, 157
forebody controls, 160, 161
thrust vector control, 159
unsteady aerodynamic effects, 158, 159
vortex effects, 161
Supermarine Spitfire, 41–44, 82, 234
Swedish Aeronautical Research Institute, 297
sweptback wing effects on stability and control,
169–174
dihedral effect at high angles of attack, 171, 172
leading edge devices, 172
pitching moments at stall, 172, 174
pylon effects, 173, 174
roll damping reversal, 169, 172
wing tip stall, 169–174
sweptforward wings, 288, 289
system matrix, 276
systems concept in stability augmentation design, 304
systems engineering, 43
Systems Technology, Inc., xix, 31, 32, 190, 192, 263,
266, 276, 319
Szalai, Kenneth, 315, 355
T-tails, 133, 136, 209–211
tactical airplane maneuverability, 146–161
tail surface size, 91, 92
Taylor, H. D., 50
tensor forms of the equations of motion, 276
© Cambridge University Press www.cambridge.org
Cambridge University Press
0521021286 - Airplane Stability and Control: A History of the Technologies That Made Aviation
Possible, Second Edition
Malcolm J. Abzug and E. Eugene Larrabee
Index
More information
390 Index
Teper, Gary L., 192, 263, 279
Test Pilot School, Edwards Air Force Base, 36
Test Pilot School, Patuxent River, 36
Thayer, W. J., 81
Theodorsen, Theodore, 166
Thomas, H. H. B. M., xviii, 30, 95, 112, 355
Thompson, Floyd L., 22, 30
Thompson, Peter M., 319, 320, 326
Thorp, John, 78
three-surface aircraft, 253
thrust-vectoring, 38, 160, 322, 340
tilted thrust line, 46, 47
time-domain response requirements, 152–155
time response parameter, 154
time vector analysis, 274, 275
Tischler, M. B., 18, 40
Tobak, Murray, 130, 142
Tobie, H. N., 154
Tokyo, University of, 13
Toll, Thomas A., 63, 70, 289, 355
Tonon, Aldo, 356
Tomayko, J. E., 83
Toot, Louisa C.,
Toronto, University of, 53
Townsend, Guy, 291
trailing edge angle, 66–68
Transall, Arbeitsgemeinschaft, 226
transfer function model for unsteady flow, 158, 159,
228, 229
transfer functions, 33, 148–152, 305
transfer function dipoles, 310
transfer function numerators, 139, 192, 193, 310
transition equations and matrices, 276
Trevelyan, A., 264
trim changes due to flaps and power, 242
Tristrant, D., 130
　
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