Development of Infrared-Guided Missile Precision Detection Simulator
Abstract
:1. Introduction
2. Device Design Based on Infrared Guided Missile Detection
2.1. Overall Structural Design of the Detection Device
2.2. Design of Rotating Device of Detection Device
2.3. Design of Lens Mechanism of Detection Device
2.4. Design of Optical System of Detection Device
2.4.1. Scheme Design of Rotating Radiation Source
- (1)
- It can balance the blackbody and reach a balanced state;
- (2)
- It can be used as an interference source to test the ability of the seeker to hit the target under the influence of low temperature interference;
- (3)
- It can be used as a radiation source at low temperatures to test other types of missiles.
2.4.2. Scheme Design of Light Path
2.5. Design of Control System for Detection Device
2.6. Working Principle of Target Simulator
3. Eccentricity and Error Analysis of Infrared Guided Missile Detection Device
3.1. Analysis of Eccentricity of Detection Device Cantilever
3.2. Modeling and Solving of Translation Distance and Tilt Angle
3.2.1. Calculation of Translational Distance and Tilt Angle
3.2.2. Kinematics Modeling of Translation and Tilt
3.3. Aberration Analysis and Calculation of Eccentric and Tilt Systems
3.3.1. Computational Analysis of Coma
3.3.2. Computational Analysis of Astigmatism
3.4. Optical Transfer Function to Evaluate Imaging Quality
3.5. Diffraction Problem Analysis
4. Experimental Study of Infrared Guided Missile Detection Device
4.1. Construction of the Body Structure of the Detection Device
4.2. Detection Device Hardware System Construction
4.3. Detection Device Rotation and Swing Operation Experiment
4.3.1. Positioning before Mechanism Experiment
4.3.2. Mechanism Movement Range Test
4.4. Verification of Rotation Angle
4.5. Detection Device Vibration Resistance Stability Swing Experiment
5. Conclusions
Author Contributions
Funding
Data Availability Statement
Conflicts of Interest
Nomenclature
Acronyms/Symbols | Explanation |
MTF | Modulation Transfer Function |
DC | Direct Current |
λ | Wavelength |
y | The distance between the blackbody and the central axis |
l1 | Entrance pupil diameter |
l2 | Exit pupil diameter |
F | F-number |
ω | The field angle |
ZEMAX | Optical design software |
PLC | Programmable logic controller |
ωmax | Maximum deflection |
θmax | Angle |
E | Modulus of elasticity |
I | Moment of inertia |
D-H | Denavit-Hartemberg [26] |
DOF | Degree of freedom |
The incident angle | |
Meridian coma aberration | |
The sagittal coma | |
The meridional image point | |
The sagittal image point | |
The axial distance of the refraction point M of the principal ray on the sphere relative to | |
The axial distance of the refraction point M of the principal ray on the sphere relative to | |
The axial distance of the refraction point M of the principal ray on the sphere relative to | |
The axial distance of the refraction point M of the principal ray on the sphere relative to | |
The meridian field area | |
The sagittal field area | |
Astigmatism | |
θ | The dispersion angle |
The angular diameter of Airy spot | |
δl | The line diameter |
f’ | Focal length |
RS232 | Recommeded standard 232 |
DSP | Digital Signal Processing |
FOC | Field-oriented control |
PNP | P-N-P |
PI | Purse input |
DO | Digital output |
MiniUSB | Mini UniversalSerialBUS |
LabVIEW | A program development environment developed by NATIONAL Instruments (NI) |
VISA | Virtual Instrument Software Architecture |
ARM | Advanced RISC Machines |
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Joint i | ||||
---|---|---|---|---|
1 | 0 | 0 | 0 | |
2 | 0 | 0 | ||
3 | 0 | 0 | ||
4 | 0 | 0 |
Direction | Frequency Range (Hz) | Total Square Root Acceleration (g) | Spectral Density (g2/Hz) | Vibration Time (s) |
---|---|---|---|---|
Y | 20~2000 | 5 | 0.028 | 12 |
X | 20~2000 | 7.6 | 0.0628 | 12 |
Test Conditions | |||||
---|---|---|---|---|---|
Frequency (Hz) | Amplitude (mm) | Acceleration (m/s2) | Test Duration (min) | ||
X axis | Y axis | Z axis | |||
(10 ± 2) | (2.0 ± 0.3) | ||||
(20 ± 2) | (1.0 ± 0.15) | ||||
(30 ± 2) | (0.8 ± 0.12) | ||||
(40 ± 2) | (0.6 ± 0.19) | ||||
(50 ± 2) | (0.4 ± 0.06) | (10 ± 1) | 5 | 5 | |
(60 ± 2) | (0.3 ± 0.04) | ||||
(80 ± 2) | (40 ± 8) | ||||
(100 ± 2) | |||||
(120 ± 2) |
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Wang, Z.; Wu, Z.; Wang, T.; Zhang, B. Development of Infrared-Guided Missile Precision Detection Simulator. Machines 2021, 9, 198. https://doi.org/10.3390/machines9090198
Wang Z, Wu Z, Wang T, Zhang B. Development of Infrared-Guided Missile Precision Detection Simulator. Machines. 2021; 9(9):198. https://doi.org/10.3390/machines9090198
Chicago/Turabian StyleWang, Zhuo, Zhenyu Wu, Tao Wang, and Bo Zhang. 2021. "Development of Infrared-Guided Missile Precision Detection Simulator" Machines 9, no. 9: 198. https://doi.org/10.3390/machines9090198