In this paper, two points guidance law of a missile is optimized based on the gravitational search algorithm. For this purpose, first, a five-degree-of-freedom equations of the missile and target are modeled. The proportional guidance law is, then, simulated to track the target. In the next step, the parameters of the law guidance are optimized using the gravitational search algorithm. Finally, the movement path of the missile and target on the horizon and vertical plane, acceleration commands, as well as the miss distance are shown. Also, the effect of axial acceleration compensation, gravitational compensation, updated frequency on the acceleration commands, the seeker's range as well as the maximum rate of seeker are investigated on the guidance law.
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Bayat Tajvar,R. , Soleimani Malekan,M. and Salehi Shaygan,A. (2019). Optimizing the Parameters of the Missile Tactical Guidance Law based on the Heuristic Gravitational Search Algorithm. Journal of Aeronautical Engineering, 21(2), 29-35.
MLA
Bayat Tajvar,R. , , Soleimani Malekan,M. , and Salehi Shaygan,A. . "Optimizing the Parameters of the Missile Tactical Guidance Law based on the Heuristic Gravitational Search Algorithm", Journal of Aeronautical Engineering, 21, 2, 2019, 29-35.
HARVARD
Bayat Tajvar R., Soleimani Malekan M., Salehi Shaygan A. (2019). 'Optimizing the Parameters of the Missile Tactical Guidance Law based on the Heuristic Gravitational Search Algorithm', Journal of Aeronautical Engineering, 21(2), pp. 29-35.
CHICAGO
R. Bayat Tajvar, M. Soleimani Malekan and A. Salehi Shaygan, "Optimizing the Parameters of the Missile Tactical Guidance Law based on the Heuristic Gravitational Search Algorithm," Journal of Aeronautical Engineering, 21 2 (2019): 29-35,
VANCOUVER
Bayat Tajvar R., Soleimani Malekan M., Salehi Shaygan A. Optimizing the Parameters of the Missile Tactical Guidance Law based on the Heuristic Gravitational Search Algorithm. JoAE, 2019; 21(2): 29-35.
