Spacecraft Dynamics and Control: A Practical Engineering ApproachSatellites are used increasingly in telecommunications, scientific research, surveillance, and meteorology, and these satellites rely heavily on the effectiveness of complex onboard control systems. This book explains the basic theory of spacecraft dynamics and control and the practical aspects of controlling a satellite. The emphasis throughout is on analyzing and solving real-world engineering problems. For example, the author discusses orbital and rotational dynamics of spacecraft under a variety of environmental conditions, along with the realistic constraints imposed by available hardware. |
Contents
III | 1 |
IV | 2 |
V | 3 |
VI | 5 |
VII | 7 |
IX | 8 |
X | 9 |
XI | 10 |
CXVI | 167 |
CXVII | 169 |
CXVIII | 172 |
CXIX | 185 |
CXXI | 186 |
CXXII | 188 |
CXXIII | 189 |
CXXIV | 190 |
XII | 11 |
XIII | 12 |
XV | 15 |
XVI | 18 |
XVII | 19 |
XVIII | 20 |
XIX | 22 |
XX | 24 |
XXI | 26 |
XXII | 27 |
XXIII | 28 |
XXIV | 29 |
XXV | 30 |
XXVI | 33 |
XXIX | 34 |
XXX | 39 |
XXXI | 41 |
XXXII | 42 |
XXXIII | 43 |
XXXIV | 45 |
XXXV | 50 |
XXXVI | 56 |
XXXVII | 57 |
XXXIX | 58 |
XL | 62 |
XLII | 64 |
XLIII | 65 |
XLVI | 68 |
XLVII | 69 |
XLVIII | 70 |
L | 71 |
LI | 72 |
LII | 73 |
LIII | 76 |
LIV | 78 |
LV | 80 |
LVI | 81 |
LVII | 84 |
LVIII | 85 |
LIX | 86 |
LXI | 88 |
LXII | 90 |
LXIV | 91 |
LXV | 93 |
LXVI | 95 |
LXVIII | 96 |
LXIX | 97 |
LXX | 98 |
LXXI | 99 |
LXXII | 100 |
LXXIII | 101 |
LXXIV | 102 |
LXXV | 104 |
LXXVII | 105 |
LXXVIII | 107 |
LXXIX | 108 |
LXXX | 111 |
LXXXII | 112 |
LXXXIII | 113 |
LXXXIV | 114 |
LXXXVI | 117 |
LXXXVII | 122 |
LXXXVIII | 126 |
LXXXIX | 129 |
XCI | 130 |
XCII | 132 |
XCIII | 135 |
XCIV | 137 |
XCV | 139 |
XCVI | 140 |
XCVII | 141 |
XCVIII | 144 |
C | 146 |
CI | 148 |
CIII | 150 |
CIV | 151 |
CVI | 152 |
CVII | 153 |
CVIII | 155 |
CIX | 156 |
CXI | 158 |
CXII | 160 |
CXIII | 161 |
CXIV | 164 |
CXV | 165 |
CXXV | 192 |
CXXVI | 195 |
CXXVII | 197 |
CXXVIII | 201 |
CXXX | 206 |
CXXXI | 208 |
CXXXIII | 210 |
CXXXIV | 214 |
CXXXV | 215 |
CXXXVI | 217 |
CXXXVII | 222 |
CXXXVIII | 225 |
CXXXIX | 229 |
CXL | 230 |
CXLI | 233 |
CXLII | 237 |
CXLV | 238 |
CXLVI | 240 |
CXLVII | 241 |
CXLVIII | 242 |
CL | 244 |
CLI | 246 |
CLII | 247 |
CLIII | 248 |
CLIV | 250 |
CLV | 251 |
CLVI | 256 |
CLVII | 257 |
CLVIII | 260 |
CLIX | 261 |
CLX | 263 |
CLXI | 265 |
CLXII | 266 |
CLXIII | 270 |
CLXIV | 273 |
CLXV | 287 |
CLXVI | 289 |
CLXIX | 291 |
CLXX | 292 |
CLXXI | 296 |
CLXXII | 299 |
CLXXIII | 301 |
CLXXIV | 302 |
CLXXV | 308 |
CLXXVI | 309 |
CLXXVIII | 310 |
CLXXX | 311 |
CLXXXI | 312 |
CLXXXII | 313 |
CLXXXIII | 316 |
CLXXXV | 318 |
CLXXXVI | 319 |
CLXXXVII | 320 |
CLXXXVIII | 322 |
CLXXXIX | 323 |
CXC | 324 |
CXCI | 325 |
CXCII | 326 |
CXCIV | 328 |
CXCV | 329 |
CXCVII | 330 |
CXCVIII | 339 |
CXCIX | 343 |
CC | 345 |
CCI | 351 |
CCII | 353 |
CCIII | 357 |
CCIV | 366 |
CCV | 373 |
CCVI | 375 |
| 376 | |
CCVIII | 379 |
CCIX | 381 |
CCXI | 382 |
CCXII | 385 |
CCXIII | 387 |
CCXIV | 388 |
CCXV | 392 |
CCXVI | 393 |
CCXVII | 396 |
CCXIX | 397 |
CCXX | 398 |
| 401 | |
| 403 | |
Other editions - View all
Spacecraft Dynamics and Control: A Practical Engineering Approach Marcel J. Sidi Limited preview - 2000 |
Spacecraft Dynamics and Control: A Practical Engineering Approach Marcel J. Sidi No preview available - 1997 |
Common terms and phrases
acceleration accuracy achieved amplitude angular momentum angular velocity apogee arc degrees attitude control attitude control system attitude determination attitude error attitude maneuvers axis frame body axes command components control law control loop control torques cos(a defined denutation dipole earth sensor eccentricity eccentricity vector Euler angles example external disturbances feedback follows frequency fuel geostationary orbit gyros hardware impulse inclination vector kg-mē linear located magnetic torqrods mode modulator moments of inertia momentum bias momentum exchange devices momentum wheel nutation open-loop orbit output parameters perigee pitch plane products of inertia propulsion pulse quaternion rad/sec reaction thrusters reaction wheel reference frame roll rotation satellite's scanning Section sensor noise shown in Figure sin(a sloshing solar panels space spacecraft spin stability star sensor sun sensors thrust tion torque torque control transfer function transformation velocity vector w₁ yaw angle ZB axis


