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Non-driven Micromechanical Gyroscopes and Their Applications
von: Fuxue Zhang, Wei Zhang, Guosheng Wang
Springer-Verlag, 2017
ISBN: 9783662540459 , 367 Seiten
Format: PDF, Online Lesen
Kopierschutz: Wasserzeichen
Preis: 96,29 EUR
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Preface
5
About the Book
7
Contents
8
Author’s Introduction
13
Non-driven Mechanical Gyroscopes
15
1 Operating Theory of a Non-driven Mechanical Gyroscope
16
1.1 Characteristics of a Flying Aircraft
16
1.2 Motion Equation for the Sensitive Elements in a Non-driven Mechanical Gyroscope
22
1.3 Performance of the Gyroscope as the Aircraft Rotates With a Constant Angular Velocity
29
1.4 Choice of System Scheme for a Non-driven Mechanical Gyroscope
32
1.5 Dynamic Performance Regulation of the System
40
1.6 Stability of a Non-driven Mechanical Gyroscope with Negative Velocity Feedback
48
1.7 Technical Performance of a Non-driven Mechanical Gyroscope
69
2 Precision of a Non-driven Mechanical Gyroscope with Negative Velocity Feedback
71
2.1 Measurement Precision of a Constant Angular Velocity Rotating Around The Horizontal Axis
71
2.2 Regulation of a Non-driven Mechanical Gyroscope
92
3 Performances of Non-driven Mechanical Gyroscope in the Condition of an Alternating Angular Velocity
97
3.1 Performance of Non-driven Mechanical Gyroscope in the Condition of an Angular Vibration
98
3.2 Output Signal of Non-driven Mechanical Gyroscope in the Condition of an Angular Vibration
112
3.3 Measurement Accuracy of the Harmonic Angular Velocity for the Aircraft
117
3.4 Performance of Non-driven Mechanical Gyroscope in a Circumferential Vibration
141
4 The Operating Errors of a Non-driven Mechanical Gyroscope
148
4.1 Error Caused by Static Unbalance of the Framework
148
4.2 Error Caused by Angular Vibration and Circumferential Vibration
152
4.3 Error Caused by Imprecise Installation
154
4.4 Error Caused by Change of Environmental Temperature
157
Non-driven Micromechanical Gyroscopes
162
5 The Micromechanical Accelerometer and the Micromechanical Gyroscope
163
5.1 The Micromechanical Accelerometer
163
5.1.1 Basic Principle, Technology Type and Applications of a Micromechanical Accelerometer
163
5.1.2 The Working Principle of a Micromechanical Accelerometer
166
5.1.3 The Micromechanical Accelerometer Manufactured by a Bulk Micromachining Process
167
5.1.4 The Micromechanical Accelerometer Manufactured by a Surface Micromachining Process
171
5.1.5 Force Feedback
176
5.1.6 The Resonant Micromechanical Accelerometer
178
5.2 The Micromechanical Gyroscope
181
5.2.1 The Structural Basis of a Micromechanical Gyroscope
181
5.2.2 The Basic Principle of a Micromechanical Gyroscope
183
5.2.3 Frequency Bandwidth
186
5.2.4 Thermal Mechanical Noise
189
5.2.5 Types of Micromechanical Gyroscope
190
6 The Working Principle of a Non–Driven Micromechanical Gyroscope
197
6.1 The Structure Principle
197
6.2 The Dynamic Model
198
6.2.1 The Mass Vibrational Model
198
6.2.2 The Solution of the Angular Vibrational Equation
203
6.3 Analysis and Calculation of Kinetic Parameters
206
6.3.1 Torsion Stiffness of the Elastic Supporting Beam
206
6.3.2 Parameter Calculation of the Flexible Joints
207
6.3.3 The Damping Coefficient of Angular Vibration for the Vibrating Element
209
6.3.4 Relationship Between the Angular Vibration Natural Frequency, the Angular Vibration Amplitude and the Measured Angular Velocity
211
6.4 Signal Detection
212
6.4.1 The Relationship Between the Output Voltage and The Swing Angle
213
6.4.2 Signal Processing Circuit
215
6.5 ANSYS Simulation and Analogy
220
6.5.1 Modal Analysis
220
6.5.2 Frequency Response Analysis
221
7 Error of a Non-driven Micromechanical Gyroscope
223
7.1 Motion Equations of a Vibratory Gyroscope
223
7.2 Error Principle of a Vibratory Gyroscope
234
7.3 Error Calculation of a Non-driven Micromechanical Gyroscope
240
7.4 Error of a Non-driven Micromechanical Gyroscope
243
8 Phase Shift of a Non-driven Micromechanical Gyroscope
246
8.1 Phase Shift Calculation of a Non-driven Micromechanical Gyroscope
246
8.2 Phase Shift of a Non-driven Micromechanical Gyroscope
250
8.3 Feasibility of Adjusting the Position to Compensate the Phase Shift of the Output Signal
252
8.4 Characteristic Calculation of a Non-driven Micromechanical Gyroscope in the Angular Vibration Table
256
9 Static Performance Test of a Non-driven Micromechanical Gyroscope
260
9.1 Performance of the Prototype of a Non-driven Micromechanical Gyroscope
260
9.1.1 Temperature Performance of the Prototype
260
9.1.2 Performance of the Prototype
263
9.1.3 Temperature Stability of the Prototype
265
9.2 Performance of a CJS-DR-WB01 Type Silicon Micromechanical Gyroscope
266
9.3 Performance of a CJS-DR-WB02 Type Silicon Micromechanical Gyroscope
267
9.4 Performance Test of CJS-DR-WB03 Type Silicon Micromechanical Gyroscope
267
Applications of Non-driven Micromechanical Gyroscopes
291
10 Signal Processing
292
10.1 Inhibiting the Influence of a Change in Rolling Angular Velocity of the Rotating Body on the Stability of the Output Signal
292
10.1.1 Influence of a Change in Rolling Angular Velocity of the Rotating Body on the Output Signal
292
10.1.2 Method for Inhibiting the Influence of a Change in Rolling Angular Velocity on the Output Signal
292
10.1.3 Validation of Inhibiting Influence Method
295
10.2 The Attitude Demodulation Method of a Micromechanical Gyroscope Based on Phase Difference
299
10.2.1 Study of the Phase Difference Between the Output Signal and the Reference Signal of the Gyroscope
299
10.2.2 Factors Influencing Phase Difference
307
10.2.3 Phase Difference Compensating Method
314
10.3 Posture Demodulation of the Rotating Body Based on the Micromechanical Gyroscope
317
10.3.1 Demodulation Method
317
10.3.2 Simulation Experiment
328
11 Applications in the Flight Attitude Control System
331
11.1 Calculation Method Design and Software Creation
331
11.1.1 Calculation Method and Software
331
11.1.2 Computer Software Design
331
11.2 Influence Connected Motion (Angular Vibration) as Three Axes Move Simultaneously
335
11.3 DSP Digital Output of the Gyroscope
336
11.3.1 Hardware Circuit Design
336
11.3.2 Algorithm and Software Realization
337
11.3.3 Test Results
340
11.4 Attitude Sensing System for Single Channel Control of the Rotating Flight Carrier
343
11.5 Three Channels Attitude Sensing System of the Rotating Flight Carrier Through the Rectangular Coordinate Transformation
346
11.6 Attitude Sensing System of the Rotating Flight Carrier Through the Polar Coordinate Transformation
350
11.6.1 Method for Obtaining the Transverse Angular Velocity Relative to the Rotating Coordinate System of the Rotating Flight Carrier
352
11.6.2 Method for Obtaining the Rolling Angular Velocity Relative to the Coordinate System of the Quasi-Rotating Flight Carrier
354
11.6.3 Method for Obtaining the Pitch Angular Velocity and the Yaw Angular Velocity Relative to the Coordinate System of the Quasi-Rotating Flight Carrier
356
11.7 Applications in the Non-rotating Flight Carrier
357
References
359