An Example of a Special Algorithm Application for Control of Aerial Guided Bomb Flight, during Guidance on the Ground Moving Target

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This paper presents the analysis of the variety of methods regarding aerial guided bomb control during the ground attack on a moving target. Based on this method there was an earlier research regarding motion control of the three degrees of freedom gyroscope axis [1,2] during space exploration and discovered target tracking. Positive results obtained during that research led to conclusion that the proposed control method will be accurate to establish a control force for aerial bomb guiding. This method is based on the use of phase trajectories control deviations. Switching of the control forces in the particular phase plane points causes the deviations to decrease to zero and facilitates the proper trajectory of the bomb. This paper presents a switching algorithm, equations of kinematics and dynamics of a bomb flight-path and the variety of examples of a numerical simulations. Obtained results were presented in the graphic form.

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93-103

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January 2016

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[1] J.C. Hsu, A.U. Meyer: Modern Control Principles and Application, McGraw-Hill, New York (1968).

Google Scholar

[2] J.W. Osiecki, K. Stefański: On a Method of Target Detection and Tracking Used in Air Defence, Journal of Theoretical and Applied Mechanics, Vol. 46, Issue 4, pp.909-916, Warsaw (2008).

Google Scholar

[3] R. Yanushevsky: Guidance of Unmanned Aerial Vehicles, Taylor & Francis Group, New York, (2011).

Google Scholar

[4] D. Gapiński, Z. Koruba and I. Krzysztofik: The Model of Dynamics and Control of Modified Optical Scanning Seeker in Anti-Aircraft Rocket Missile, Mechanical Systems and Signal Processing, Vol. 45, issue 4, pp.433-447, (2014).

DOI: 10.1016/j.ymssp.2013.11.016

Google Scholar

[5] Z. Koruba: Optimal Control of the Searching and Tracking Head (STH) for Self Propelled Anti Aircraft Vehicle, Solid State Phenomena, Vol. 180, pp.27-38, Trans Tech Publications, Switzerland (2012).

DOI: 10.4028/www.scientific.net/ssp.180.27

Google Scholar

[6] Z. Dziopa, P. Buda, M. Nyckowski and R. Pawlikowski: Dynamics of an Unguided Missiles Launcher, Journal of Theoretical and Applied Mechanics, Vol. 53, Issue 1, (2015).

DOI: 10.15632/jtam-pl.53.1.69

Google Scholar

[7] Z. Koruba, Ł. Nocoń: Automatic Control of an Anti-Tank Guided Missile Based on Polinomial Functions, Journal of Theoretical and Applied Mechanics, Vol. 53, Issue 1, pp.139-150, Warsaw (2015).

DOI: 10.15632/jtam-pl.53.1.139

Google Scholar

[8] K. Stefański, Z. Koruba: Analysis of the Guiding of Bomb On Ground Targets Using a Gyroscope System, Journal of Theoretical and Applied Mechanics, Vol. 50, Issue 4, pp.967-973, Warsaw (2012).

Google Scholar

[9] Z. Koruba, Z. Dziopa, I. Krzysztofik: Dynamics and Control of a Gyroscope-Stabilized Platform in a Self-Propelled Anti-Aircraft System, Journal of Theoretical and Applied Mechanics, Vol. 48, Issue 1, pp.5-26, Warsaw (2010).

Google Scholar

[10] Z. Koruba, J.W. Osiecki: Constructions, Dynamics and Navigation of the Short Range Rocket Missile (in polish), 1st part, Academy Course Book, No. 348, Kielce University of Technology, 1999).

Google Scholar

[11] A. Żyluk: Sensitivity of a Bomb To Wind Turbulence, Journal of Theoretical and Applied Mechanics, Vol. 47, Issue 4, pp.815-828, Warsaw (2009).

Google Scholar