SYSTEM FOR INFORMATION SUPPORT OF INTERACTION IN AIRCRAFT GROUP

aircraft board equipment. SUBSTANCE: device has inertial satellite coordinate detector, unit for data reception and transmission, target coordinate detector, relative coordinate generator. Goal of invention is achieved by introduced delay gate, error separation unit, optimal filtering unit, correcti...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
Hauptverfasser:	DZHANDZHGAVA G.I, BEKETOV V.I, SIMONOV M.P, SUKHORUKOV S.JA, EVDOKIMOV G.I, GERASIMOV G.I, PANKOV O.D, OREKHOV M.I, ROGALEV A.P, MOISEEV A.G, BRAZHNIK V.M, KORCHAGIN V.M, NEGRIKOV V.V
Format:	Patent
Sprache:	eng
Schlagworte:	GYROSCOPIC INSTRUMENTS MEASURING MEASURING DISTANCES, LEVELS OR BEARINGS NAVIGATION PHOTOGRAMMETRY OR VIDEOGRAMMETRY PHYSICS SIGNALLING SURVEYING TESTING TRAFFIC CONTROL SYSTEMS
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Beschreibung
Zusammenfassung:	aircraft board equipment. SUBSTANCE: device has inertial satellite coordinate detector, unit for data reception and transmission, target coordinate detector, relative coordinate generator. Goal of invention is achieved by introduced delay gate, error separation unit, optimal filtering unit, correction generation unit, and unit for generation of parametric functions. EFFECT: increased precision of relative navigation and target setting parameters, generation of target setting parameters, when an aircraft in group misses contact to target, increased functional capabilities, improved warfare performance of aircraft group. 1 dwg