METHOD FOR TESTING THE ROCKET CONTROLLED IN LASER RAY

This invention relates to rocket technique and can be used in complexes of arms to which rockets controlled by means of laser ray are included. Method for testing the rocket comprises of formation of support trajectory of the rocket as a fixed aimingline, with formation of control command proportion...

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Hauptverfasser: KOSOVENKO YEVHEN VIKTOROVYCH, SEMENOV LEONID ANTONOVYCH, EGLIT MYKOLA OLEKSANDROVYCH, SMISHKO GRYGORII PAVLOVYCH, DOTSENKO BORYS IVANOVYCH, KUZMIN VIACHESLAV PAVLOVYCH, KOROLIOV ANATOLII MYKOLAIOVYCH, KOROSTELIOV OLEG PETROVYCH, YAKOVENKO PETRO OLEKSIIOVYCH
Format: Patent
Sprache:eng
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Zusammenfassung:This invention relates to rocket technique and can be used in complexes of arms to which rockets controlled by means of laser ray are included. Method for testing the rocket comprises of formation of support trajectory of the rocket as a fixed aimingline, with formation of control command proportional to deflection of the rocket from the center of the laser ray, with aiming the rocket with application of control command, transmission and receipt of telemetric information on deflection of the rocket from the center of the laser ray, estimation of linear disagreement between the rocket and the basic trajectory of aiming. Additionally one determines the current deflection of the laser ray with respect to the aiming. The current linear disagreement between the rocket and the basic trajectory of aiming is determined through comparing telemetric data on the current deflection of the rocket from the center of the laser ray and the data of the receiver of the laser ray on the current deflection of the laser ray from the fixed aiming line. The level of registered deflection estimates quality of the process of stabilization of the rocket in information field of control.