High-precision, stable tracking technology on a mobile platform is a key technology for realizing the integration of airborne search and tracking. In this study, coarse-fine compound technology based on gyrostabilization and miss tracking is applied. First, the working principle of the coarse and fine composite system is analyzed, and then the coarse and fine composite algorithm is modeled. Thereafter, the error of the coarse and fine composite axis is analyzed, and the precision tracking servo control algorithm is designed. Finally, using the model and algorithm designed to control the single reflector and galvanometer, the coarse tracking of the space target and the fine tracking of the source are completed under the condition that the equivalent sine amplitude is 5 deg and the frequency is 0.2 Hz. At the same time, a test system was built for performance verification. The algorithm achieved a coarse-tracking azimuth-axis tracking accuracy [root mean square (RMS)] of 26.3 μrad and a pitch-axis tracking accuracy (RMS) of 28.9 μrad. After composite tracking was switched on, precision tracking azimuth-axis tracking accuracy (RMS) improved to 7.9 μrad and pitch-axis tracking accuracy (RMS) improved to 6.3 μrad, both better than 10 μrad. This study provides new insights into the stability and precision tracking of single cameras on airborne platforms. At the end of this work, the outdoor experiment to verify the influence of random interference on the system performance under given conditions and the subsequent optimization direction of the system are given.
This paper focuses on the embedded laser target simulation system based on RTX(Real Time Executive).This system completes the seeker test mission mainly by means of simulating the process of the missile from launch to hit the target through controlling the Laser spot. The system is consisted of upper computer, spot energy adjustment and spot size adjustment. The whole system realizes continuous and rapid adjustment to the energy and size of the spot via the RTX embedded computer system sends control commands to each controller of two units simultaneously. The unit of spot size adjustment: the controller controls the movement of the leading screw and then the leading screw controls the shift of the lens. The motor which controls the movement of the leading screw is direct current torque motor. The unit of spot energy adjustment: According to the Lambert law, the structure uses two crystals that the wedge angles are exactly the same. The system controls the motor to change the relative position of these crystals and then changes the thickness of the optical path crystal to adjust the laser spot energy. This system utilizes RTX embedded system to send control commends s in real time, a share memory area is opened for exchanging the simultaneous data between Windows and RTX. The real-time performance of the whole system has a significantly improve by using RTX embedded system, the system response time reduces to 1ms。Thus the laser target achieves rapid changing which seeker test requirement.
The intelligent control of simulation target with infrared imaging target in the indoor and outdoor
environment can effectively and quantitatively evaluated the parameters such as the minimum resolution
temperature difference(MRTD)and spatial resolution of airborne forward looking infrared, infrared detection
and tracking, infrared alarm, and etc.
This paper focused on introducing the working principles of the intelligent control simulation target of
Infrared imaging target, studying the thermal radiation characteristics of the infrared target surface material,
analyzing the influences of the infrared radiation energy distribution, and developing the intelligent control
simulation target with IR imaging target for hardware-in-the-loop simulation test. The intelligent control
simulation target which area was 5 ㎡ and concluded 44 infrared targets including two kinds of infrared
targets ,0.25m×0.25m, and 0.25m×0.5m, achieved 1℃~10℃ temperature simulation of target and the
background, and temperature control precision better than 0.5℃. Field test requirements were achieved by
actual test.
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