THE USE OF SPECIAL ALGORITHM TO CONTROL THE FLIGHT OF ANTI-AIRCRAFT MISSILE
Abstract eng: The paper analyzes a possibility of using the special algorithm to control the flight of a homing air target missile. The method is based on the signum function and utilizes the phase trajectories of errors resulting from the adopted homing method (proportional navigation). The results obtained via Matlab package are presented in graphical form.
Contributors:
Publisher:
Institute of Thermomechanics AS CR, v.v.i., Praha
Conference Title:
Conference Title:
Engineering Mechanics 2016
Conference Venue:
Svratka, CZ
Conference Dates:
2016-05-09 / 2016-05-12
Rights:
Text je chráněný podle autorského zákona č. 121/2000 Sb.
Record appears in:
Record created 2016-08-16, last modified 2016-08-16
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