Fiber Optic Inertial Navigation

Fiber Optic Inertial Navigation

  • FS300-42 Optical Fiber Integrated Navigation System

    FS300-42 Optical Fiber Integrated Navigation System

    Fibra optica integrata systematis navigandi FS300-42 componitur ex levi et parvo tribus-axis integratis fibra gyroscopi optici, gyroscopi optici, accelerometer et ductor cardus innixus cost-effective.Consequitur algorithmus multi-sensorem fusionem et navigationem, ac requisitis occurrere potest ad accurate mensuras habitus, ac positio notitias in applicatione agrorum medii et magni certaminis mobilis ratio mensurae et medii et magnae UAV.

  • FS300-70 Optical Fiber Integrated Navigation System

    FS300-70 Optical Fiber Integrated Navigation System

    Fibra optica integrata systematis navigandi FS300-70 fundatur in fibra gyroscopi optici, fibra gyroscopi optici, accelerometer et summus finis GNSS recipiens, et per multi-sensorem fusionem et navigationis solutionem algorithmus perficitur.Requisitis ad accurate mensuras habitus, capitis ac positionis potest occurrere informationes in media et alta praecisione systemata mobilia mensurae, magna inanibus vehiculis aereis et aliis applicationibus.

  • FS300-98 Fiber Optic Integrated Navigation System

    FS300-98 Fiber Optic Integrated Navigation System

    Fibra optica systematis navigandi integratumFS300-98fundatum est in fibra gyroscopi optici cost-efficax clausa, accelerometer et summus finis GNSS tabulae recipiendae, per multi-sensorem fusionem et navigationem solutionem algorithmus exsequendam ad necessitates mediae et altae praecisiones systematum mobiles mensurae, magnas UAVs, etc. . Applicatio campus accurate mensuras habitus, capitis ac positionis informationes requirit.

  • FS100 Fiber Optical Strapdown Inertial / Satellite Integrated Navigation System

    FS100 Fiber Optical Strapdown Inertial / Satellite Integrated Navigation System

    FS100 fibra optica integrata systema navigandi componitur ex gyroscopo fibro-lope clauso-optico, vicus accelerometer flexibilis et summus terminus GNSS recipiens tabulam, per multi- fusionem sensorem et regimen.

    Effectio algorithmus aeria calculi, summus praecise navigandi habitus, celeritas ac positio notitias ad res extra orbem pertinentes, occurrit summus praecisio mensurae et imperium requisita.