Advanced SearchSearch Tips
Look-Angle-Control Homing Loop Design with a Strapdown Seeker and Single Gyroscope
facebook(new window)  Pirnt(new window) E-mail(new window) Excel Download
 Title & Authors
Look-Angle-Control Homing Loop Design with a Strapdown Seeker and Single Gyroscope
Hong, Ju-Hyeon; Park, Kuk-Kwon; Park, Sang-Sup; Ryoo, Chang-Kyung; Cho, Han-Jin; Cho, Young-Ki;
  PDF(new window)
In this paper, the terminal homing loop with a IIR-type strapdown seeker and a roll rate gyroscope is proposed. Basically, the proposed homing loop is based on the look-angle-control guidance. Since the range of the seeker is strictly limited, the missile is delivered to a point to lock the target on the seeker via non-guided flight during the midcourse guidance. The non-standard firing table is developed to compensate the wind and the target movement. To secure the delay margin is very important to prevent the instability of the homing loop when the time delay of the seeker is included. To validate the proposed homing loop, the 6-DOF nonlinear simulation is performed, and the Monte-Carlo simulation is also done for checking the robustness for the various kinds of uncertainty.
Look-angle Control;Strapdown Seeker;Delay Margin;
 Cited by
Nesline, F. W., and Nesline, M. L., "How autopilot requirements constrain the aerodynamic design of homing missiles". Proceeding In American Control Conference, 1984, pp. 716-730.

Blakelock, J. H., Automatic control of aircraft and missiles, John Wiley & Sons, 1991.

Kim, D., Ryoo, C. K., Kim, Y., & Kim, J., "Guidance and control for missiles with a strapdown seeker", Proceeding In 11th International Conference Control Automation and Systems (ICCAS), 2011, pp. 969-972.

Jang, S.-A., Ryoo, C.-K., Choi, K. Y., and Tahk, M.-J., "Parasite loop compensation of missile with strapdown seeker," Proceeding In the 15th Guidance Weapon Conference (in Korean), 2009, pp. 65-70.

Yun, J., Ryoo, C. K., and Song, T. L., "Guidance Filter Design Based on Strapdown Seeker and MEMS Sensors", Journal of The Korean Society for Aeronautical and Space Sciences, Vol.37, No.10, 2009, pp. 1002-1009. crossref(new window)

Oh, S. M., "Terminal Homing Guidance of Tactical Missiles with Strapdown Seekers Based on an Unscented Kalman Filter", Journal of the Korean Society for Aeronautical & Space Sciences, Vol.38, No.3, 2010, pp. 221-227. crossref(new window)

Kim, D., Park, W., & Ryoo, C. K., "Look-Angle-Control Guidance for Missiles with Strapdown Seeker", Journal of Institute of Control, Robotics and Systems, Vol.19, No.3, 2013, pp. 275-280. crossref(new window)

Kook, D. H., Fire Control System Improvement with application to Firing while Transfer for A Tracked Anti-air Gun, Master Thesis, Hanyang University, 2005.

Han, D. H., Lee, D. G., Song, T. L., and Lee, Y. J., "Study on ballistics calculation technique using numerical method", Proceedings of the 5thseminaron Naval Weapon Systems Development, Agency for Defense Development, Jinhae, 2004, pp. 300-305.

Astrom, K. J., and Richard M. M., Feedback systems: an introduction for scientists and engineers., Princeton university press, 2010.