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航天传感器(影印版)
商品编号:2295779
ISBN:9787560350578
出版社:哈尔滨工业大学出版社
作者: 亚历山大·尼拜洛夫作
出版日期:2015-06-01
开本:16
装帧:暂无
中图分类:V443
页数:384
册数:1
大约重量:614(g)
购买数量:
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库存:10
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预计72小时发货
甲虎价: 34.8 (2.9折)
原价:¥120.00
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作者简介
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《航天传感器(*版)》根据作者40多年来从事航空—航天飞行器结构试验和应变测量技术的体会,收集了国内外相关资料,以词目的形式汇编成册,以供从事航空—航天飞行器结构试验和应变测量技术,以及相应的工程结构试验和应变测量的各类技术人员参考。
SERIES PREFACE
PREFACE
ACKNOWLEDGMENTS
ABOUT THE SERIES EDITOR
ABOUT THE EDITOR
1 INTRODUCTION
1.1 General Considerations
1.1.1 Types of Aerospace Vehicles and Missions
1.1.2 The Role of Sensors and Control Systems in Aerospace
1.1.3 Specific Design Criteria for Aerospace Vehicles and their Sensors
1.1.4 Physical Principles Influencing Primary Aerospace Sensor Design
1.1.5 Reference Frames Accepted in Aviation and Astronautics
1.2 Characteristics and Challenges of the Atmospheric Environment
1.2.1 Components of the Earths Atmosphere
1.2.2 Stationary Models of the Atmosphere
1.2.3 Anisotropy and Variability in the Atmosphere
1.2.4 Electrical Charges in the Atmosphere
1.2.5 Electromagnetic Wave Propagation in the Atmosphere
1.2.6 Geomagnetism
1.2.7 The Planetary Atmosphere
1.3 Characteristics and Challenges of the Space Environment
1.3.1 General Considerations
1.3.2 Near—Earth Space
1.3.3 Circumsolar (Near—Sun) Space
1.3.4 Matter in Space
1.3.5 Distances and Time Scales in Deep Space
References

2 AIR PRESSURE—DEPENDENT SENSORS
2.1 Basic Aircraft Instrumentation
2.2 Fundamental Physical Properties of Airflow
2.2.1 Fundamental Airflow Physical Property Definitions
2.2.1.1 Pressure
2.2.1.2 Air Density
2.2.1.3 Temperature
2.2.1.4 Flow Velocity
2.2.2 The Equation of State for a Perfect Gas
2.2.3 Extension o fDefinitions: Total, Dynamic, Static, and Stagnation
2.2.4 The Speed of Sound and Mach Number
2.2.4.1 The Speed of Sound
2.2.4.2 Mach Number and Compressibility
2.2.5 The Source of Aerodynamic Forces
2.3 Altitude Conventions
2.4 Barometric Altimeters
2.4.1 Theoretical Considerations
2.4.1.1 The Troposphere
2.4.1.2 The Stratosphere
2.4.2 Barometric Altimeter Principles and Construction
2.4.3 Barometric Altimeter Errors
2.4.3.1 Methodical Errors
2.4.3.2 Instrumental Errors
2.5 Airspeed Conventions
2.6 The Manometric Airspeedlndicator
2.6.1 Manometric Airspeedlndicator Principles and Construction
2.6.2 Theoretical Considerations
2.6.2.1 Subsonic Incompressible Operation
2.6.2.2 Subsonic Compressible Operation
2.6.2.3 Supersonic Operation
2.6.3 Manometric Airspeed Indicator Errors
2.6.3.1 Methodical Errors
2.6.3.2 Instrumental Errors
2.7 The Vertical Speed Indicator (VSI)
2.7.1 VSI Principles and Construction
2.7.2 Theoretical Considerations
2.7.2.1 Lag Rate (Time Constant)
2.7.2.2 Sensitivity to Mach Number
2.7.2.3 Sensitivity to Altitude
2.7.3 VSI Errors
2.8 Angles of Attack and Slip
2.8.1 The Pivoted Vane
2.8.2 The Differential Pressure Tube
2.8.3 The Null—Seeking Pressure Tube
References
Appendix

3 RADAR ALTIMETERS
3.1 Introduction
3.1.1 Definitions
3.1.2 Altimetry Methods
3.1.3 General Principles of Radar Altimetry
3.1.4 Classification by Different Features
3.1.5 Application and Performance Characteristics
3.1.5.1 Aircraft Applications
3.1.5.2 Spacecraft Applications
3.1.5.3 Military Applications
3.1.5.4 Remote Sensing Applications
3.1.6 Performance Characteristics
3.2 Pulse Radar Altimeters
3.2.1 Principle of Operation
3.2.2 Pulse Duration
3.2.3 Tracking Altimeters
3.2.4 Design Principles
3.2.5 Features of Altimeters with Pulse Compression
3.2.6 Pulse Laser Altimetry
3.2.7 Some Examples
3.2.8 Validation
3.2.9 Future Trends
3.3 Continuous Wave Radar Altimeters
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