METHOD FOR FORMATION OF SIGNALS OF SINGLE-CHANNEL CONTROL OF AIRCRAFT ROTATING BY ROLL

The utility model relates to control systems of pilotless aircrafts. A method for formation of signals of single-channel control of aircraft rotating by roll consists in measuring the value of signal proportional to the value of deflection (??) of aircraft from prescribed trajectory with linear ampl...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
Hauptverfasser:	KOSOVENKO YEVHEN VIKTOROVYCH, SMISHKO HRYHORII PAVLOVYCH, KLIAVLIN VALERII VOLODYMYROVYCH, KOROSTELIOV OLEH PETROVYCH
Format:	Patent
Sprache:	eng
Schlagworte:	AMMUNITION BLASTING EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION HEATING LIGHTING MECHANICAL ENGINEERING WEAPONS
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Beschreibung
Zusammenfassung:	The utility model relates to control systems of pilotless aircrafts. A method for formation of signals of single-channel control of aircraft rotating by roll consists in measuring the value of signal proportional to the value of deflection (??) of aircraft from prescribed trajectory with linear amplification, obtaining as result the value of amplified signal of deflection of aircraft from prescribed trajectory (Uo). One sets the value of current threshold level of value of signal of aircraft deflection from prescribed trajectory (Uo), with obtaining as result the value of signal (Uthresh). One differentiates the value of signal of deflection (Uo), and obtains as result the value of signal proportional to gradient of value of aircraft deflection from prescribed trajectory (U1). One integrates the value of aircraft deflection from prescribed trajectory (Uo), and obtains as result signal value (U2). The value of single-channel resulting signal (U) is determined through adding to the value of signal of aircraft deflection from prescribed trajectory (Uo) the value of signal proportional to gradient of the deflection (U1), and the value of signal proportional to the value of integrated signal of that deflection (U2).