Study on Guidance Algorithm of Scene Matching based on Different Source Images for Cruise Missile

2018 ◽  
Author(s):  
Zhang Yi-Fei ◽  
Yang Hui
Keyword(s):  
Cruise Missile ◽  
Scene Matching ◽  
Guidance Algorithm

Real-Time Opto-Electronic Hybrid Joint-Transform-Correlator for Scene Matching Guidance

2012 ◽  
Vol 571 ◽  
pp. 377-381
Author(s):  
Xuan Ke Zhao ◽  
Qing Wu Zhao
Keyword(s):  
Processing System ◽  
Input Image ◽  
Cruise Missile ◽  
Joint Transform Correlator ◽  
Correlation Peak ◽  
Joint Power ◽  
Location Accuracy ◽  
Scene Matching ◽  
Hybrid Joint ◽  
Cruise Missiles

In this paper, an optoelectronic hybrid processing system for cruise missile scene matching guidance based on convolute structure Joint-Transform-Correlator(JTC) was proposed. By edge detection of input image and binaryzation processing of joint power spectrum, the system can achieve sharper correlation peak and location accuracy. Simulation calculation and optical experiments show that even in noisy background, the system can obtain excellent recognition and location performances with 16frames/s, recognition probability greater than 94%, and location accuracy better than a pixel. It is very advantageous to meet the demands of further improving performance, speed, and shoot accuracy of the cruise missiles.

ROC-based Canny algorithm for scene matching

2009 ◽  
Vol 29 (4) ◽  
pp. 1193-1196
Author(s):  
Zhao-hui YANG ◽  
Ying CHEN
Keyword(s):  
Scene Matching ◽  
Canny Algorithm

Possible U.S. SLCM (Sea Launched Cruise Missile) Negotiating Options

1983 ◽  
Author(s):  
John J. Ballantine ◽  
Ethan S. Burger
Keyword(s):  
Cruise Missile

scholarly journals Stability and Manoeuvrability Simulation of a Semi-Autonomous Submarine Free-Running Model SUBOFF with an Autopilot System

2021 ◽  
Vol 11 (1) ◽  
pp. 410
Author(s):  
Yu-Hsien Lin ◽  
Yu-Ting Lin ◽  
Yen-Jun Chiu
Keyword(s):  
Optimal Control ◽  
Experimental Tests ◽  
Degree Of Freedom ◽  
Line Of Sight ◽  
Pd Controller ◽  
Free Running ◽  
Simulation Results ◽  
Guidance Algorithm ◽  
Logic Operations ◽  
Six Degree Of Freedom

On the basis of a full-appendage DARPA SUBOFF model (DTRC model 5470), a scale (λ = 0.535) semi-autonomous submarine free-running model (SFRM) was designed for testing its manoeuvrability and stability in the constrained water. Prior to the experimental tests of the SFRM, a six-degree-of-freedom (6-DOF) manoeuvre model with an autopilot system was developed by using logic operations in MATLAB. The SFRM’s attitude and its trim polygon were presented by coping with the changes in mass and trimming moment. By adopting a series of manoeuvring tests in empty tanks, the performances of the SFRM were introduced in cases of three sailing speeds. In addition, the PD controller was established by considering the simulation results of these manoeuvring tests. The optimal control gains with respect to each manoeuvring test can be calculated by using the PID tuner in MATLAB. Two sets of control gains derived from the optimal characteristics parameters were compared in order to decide on the most appropriate PD controller with the line-of-sight (LOS) guidance algorithm for the SFRM in the autopilot simulation. Eventually, the simulated trajectories and course angles of the SFRM would be illustrated in the post-processor based on the Cinema 4D modelling.

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