An Application of a Special Method for Designating the Control Forces for the Homing of an Anti-Aircraft Missile on an Aerial Target by Use of a Method of Proportional Navigation
Journal Title: Problemy Mechatroniki. Uzbrojenie, lotnictwo, inżynieria bezpieczeństwa - Year 2018, Vol 9, Issue 4
Abstract
An analysis of application feasibility of a special method for surface-to-air missile (SAM) control during homing on an airborne target was carried out in this paper. A prior implementation of the method was motion control for a gyroscope axis with three degrees of freedom [1, 2] at the stages of spatial seeking and tracking of a detected target. The positive results obtained during that research led to a conclusion that the proposed control method would be appropriate for the determination of the control forces for missile guidance. This method consists of the application of the phase trajectories of control errors. Switching over of the control forces at suitable phase plane points reduced the control errors to zero and facilitated a proper flight path of the SAM. This paper presents a switching algorithm, equations of the kinematics and dynamics of SAM flight, and a number of examples of numerical simulations of the problem contemplated herein. The simulation results were represented in a graphic format.<br/><br/>
Authors and Affiliations
Konrad STEFAŃSKI
Keywords
Related Articles
- EP ID EP408465
- DOI 10.5604/01.3001.0012.7339
- Views 84
- Downloads 0
The Conception of the Time Fuse for Special Ammunition Fired from the RAK 120 mm Self-Propelled Mortar
In the paper the conception of new time fuse for smoke and illuminating projectiles fired from the RAK 120 mm self-propelled mortar was presented. The structure and the principles of operation of basic units of the fuse...
Chosen Issues of Military Radar Protection Against Antiradiation Missiles
The paper deals with the concept of suppression of enemy air defence with antiradiation missiles (ARM). ARM performance metrics and parameters are presented and compared. Some Anti-ARM techniques are discussed, i.e. low...
Nieliniowy model wyrzutni przeciwlotniczych pocisków rakietowych umieszczonej na pokładzie okrętu
W pracy przedstawione są elementy sformułowanego modelu wyrzutni przeciwlotniczych pocisków rakietowych umieszczonej na pokładzie okrętu. Ruch zestawu rozpatrywany jest w trójwymiarowej przestrzeni Euklidesa i w jednorod...
The Initial Velocities of Metal Plates Explosive-Driven from Asymmetric Sandwich
This paper presents modified Gurney formulas determining velocities of the explosive-driven metal plates which are parts of a flat asymmetric sandwich (AS). The modification takes into account a linear profile of the det...
Effect of Controlled Gas Nitriding on the Durability of the Barrels of Small Arms
The project research – development, implemented in a consortium: Institute of Precision Mechanics (Warsaw, Poland), Military University of Technology (Warsaw, Poland) and Small Arms Factory (Radom, Poland), studies were...