|
Introduction |
3 |
|
Chapter 1. Mathematical models and investigation methods for bound thermal and mechanical processes in sensors, devices and systems |
10 |
|
1.1. Generalized method for calculation and analysis of three-dimensional nonstationary inhomogeneous temperature fields of sensors, devices and systems |
- |
|
1.2. Method for calculation, analysis and visualization for nonstationary temperature fields of sensors, devices and systems with regard to relative motion dynamics of their structural
elements
|
34 |
|
1.3. Mathematical models and investigation methods for mechanical motion nontrivial processes of
sensors, devices and systems
|
58 |
|
Chapter 2. Thermally disturbed inertial data sensors |
84 |
|
2.1. Float gyroscopes under thermal actions |
- |
|
2.2. Dynamically tuned gyroscopes under thermal actions |
106 |
|
2.3. Electrostatic gyroscopes under thermal actions |
126 |
|
2.4. Hemispherical resonator gyroscopes under thermal actions |
138 |
|
2.5. Micromechanical gyroscopes and accelerometers under thermal actions |
155 |
|
2.6. Fiber-optic gyroscopes under thermal actions |
204 |
|
2.7. Systematization of mathematical models of thermally disturbed inertial sensors |
231 |
|
Chapter 3. Special problems of construction and investigation of mathematical models for
thermally disturbed aerospace sensors, devices and systems
|
242 |
|
3.1. Phenomenon of deterministic chaos in output signals of thermally disturbed aerospace sensors, devices and systems - general approach |
- |
|
3.2. Deterministic chaos in thermally disturbed dynamic systems with measuring and damping gyroscopes |
258 |
|
3.3. Possibility of irregular non-isothermal motion of viscous fluid in the floated suspension clearance |
276 |
|
3.4. Reversing and heating systems of temperature control for micromechanical aerospace
sensors
|
294 |
|
3.5. Non-linear dynamics of disturbed simple pendulums |
310 |
|
3.6. Influence of parametric disturbances on intrinsic properties of mechanical systems
|
324 |
|
Chapter 4. Thermally disturbed pressure and linear displacement sensors, devices and
electronic control units for aerospace vehicle orientation systems
|
333 |
|
4.1. Influence of thermal actions on the pressure sensor for aerospace vehicles |
- |
|
4.2. Linear displacement sensor for spacecrafts under thermal shock |
349 |
|
4.3. Multifunctional programmable controller for spacecraft orientation system under thermal actions |
362 |
|
4.4. Electronics unit for spacecraft orientation system under thermal actions |
372 |
|
Conclusions |
396 |
|
References |
399 |