Preview - UVS International
Transcrição
Preview - UVS International
SUMMARY • AVIBRAS UAV PAST EXPERIENCE • FINEP – SNC PROJECT • VANT RE FALCÃO – KEY POINTS • FALCÃO CHARACTERISTICS • FALCÃO TACTICAL EMPLOYMENT • FALCÃO PROJECT STATUS • FALCÃO ROADMAP • AVIBRAS UAV SYSTEMS – OBJECTIVES AVIBRAS – UAV Systems Success history • Freewing project experience • Open Architecture of Hw and Sw developed in Project VANT- SNC FINEP VANT SNC Project - Aerial Platforms NGCS - Adjustments to Different Aerial Platforms Harpia (Navy Aerial Target) Acauã (Reconnaissance) VANT Project Testbeds Common Architecture - Hw and Sw (Flexibility) System Engineering - GNCS Architecture Software Development 10 GNCS Test Campains – Over 55 Flights - Autonomous Navigation through waypoints - Over 55 pre-programmed flight paths executed Technological Chalenges • Inertial Nav. Unit – Kalman Filter SW for GPS + IMU Data Fusion ............................................................................... Concluded • Auto Pilot ................................................................................... Concluded • Remote Control .......................................................................... Concluded • Autonomous Flight ..................................................................... Concluded • SW Development (RUP, 12207, DO178B) ................................ Concluded • Real Time Operational Environment - QNX ............................... Concluded • CAN Aerospace Data Bus .......................................................... Concluded • COTS Equipment ...................................................................... Concluded • CAD Modeling ............................................................................ Concluded • Determination of Aerodynamics' Parameters ............................ Concluded FALCÃO UAV SYSTEMS FALCÃO UAV SYSTEMS FALCÃO - PERFORMANCE FALCÃO - PERFORMANCE FALCÃO - PERFORMANCE • Operational Range: - 2500 km (SATCOM) -150 km (LOS); • Payload: 150 kg; • Ceiling: 15.000 ft; • Endurance: 15 h; • Day and night operation using 600m long runway; • Two hard points for 50 kg in each semi-wing; • Integration of sensors for ISTAR (Intelligence, Surveillance, Target Acquisition and Reconnaissance): - Electro-optical with Laser Range Finder; - SAR/ISAR/GMTI Radar; - Satellite Link (SATCOM). • Radar + EO Turret + SATCOM in the same mission • ATOL – Automatic Take off and Landing based on Radar Altimeter/DGPS FALCÃO – CARACTHERISTCS FALCÃO – PROJECT STATUS SUMMARY - System and Components Design – Concluded - Electronic Hw and Cabling Design - 90% - System SW and AIR Version First Flight – 90% - Electronic System Components – In House - Tools for Carbon Fiber Parts – 95% - Carbon Fiber parts – 90% - Metallic Components – 90% - First Flight Campaign Planning – 70% - Ground Structural Tests with DCTA – Initiated FALCÃO – LAYOUT Canopi 1 (SATCOM / CBRN) Access Door Antennas / Others Access Door (Ballistic Parachute / Others) Access Door (SAR / SATCOM / Others) Access Door Servos e Actuators EO/IR Interface General Interface (EO/IR / Outros) Access Door Servos e Actuators Inferior Nacele (Engine / Others) FALCÃO – AERONAUTIC DESIGN FALCÃO – AERONAUTIC DESIGN FALCÃO – TOOLING AND COMPOSITE PARTS FALCÃO – TOOLING AND COMPOSITE PARTS FALCÃO - ENGINE SUPPORT TEST DCTA JIG INTERFACE PLATE INTERFACE BETWEEN ENGINE SUPPORT AND DCTA TEST JIG TEST LOAD INTERFACE FALCÃO - BRAKE SYSTEM BENCH TEST 1 – COMMMERCIAL STEEL BENCH TEST STRUCTURE ALREADY IN HOUSE; 2 – 2400 RPM MOTOR FOR WHEEL DRIVING IN HOUSE; 3 – SAME BRAKING SYSTEM MECHANISM AS THE ONE USED IN THE PROTOTYPE, IN PRODUCITION; 4- BENCH DESIGN 80% CONCLUDED. FALCÃO - VANT SUBSYSTEMS DESIGN QTTY SUBSYSTEMS / TEST BENCHES AND TOOLS 1200 1070 1000 800 TOTAL SUBSYSTEMS PRODUCT 600 600 TEST BENCHES INTEGRATION TOOLS PRODUCTION TOOLS 400 220 190 200 60 0 1 FALCÃO - HW ARCHITECTURE AERONAVE (Sensores/Atuadores) MOTOR - Rotax 912UL Ignição(x2)+Magneto Corte Ignição Partida SIST COMBUST Tanque Bomba Elétrica Aliment Válvula Corte Comb Bombas Alijamento (3) Válvulas Alijamento SIST GERAÇÃO Gerador 12V Bateria 12V Gerador 28V (x2) Bateria 28V (x2) SIST ILUM EXTERNA Luzes Naveg/Pos (x3) Luzes AC Strobe (x3) Trigger Strobe Luzes AC RotBeac(x2) Faróis Aterris (x2) Instrumentação e Comandamento Propulsor (ICP) AIR-Serial IPSE (CAIXA) AERONAVE (Sensores) Pitot Est GPS1 (Ant) MONIT&COMANDAMENTO Single Board Computer (SBC) Relay Output(x2) Power Supply Unit (PSU) ET1 ET2 RS-232 CENTRAL INERCIAL DUAL COND SINAL RDAC - MGL RELÉS RD 1 (EXPANSÃO) ET1 ET2 (EXPANSÃO) ET1 ET2 ET1 ET2 OAT Alpha/Beta GPS2 (Ant) RD 2 RS-422 (x2) - NDI + EAI / WOW (x1) AIR-Serial CDB-A Single Board Computer (SBC) 2 x CAN Interface Power Supply Unit (PSU) Mini-Boom Interface A AERONAVE (SOBRE O TANQUE DIANTEIRO) AIR-Serial RS-422 (x2) - NDI + EAI / WOW (x1) CAN-1 CAN-2 AERONAVE CAN-1 CAN-2 MICAN V3 RS-xxx DATA-LINK TM-TC VHF (EMETG) ANTENAS & COMB RM-1 (UP-A) RS (2) RM-2 (UP-B) RS (2) RM-3 (DOWN) RS (2) FDR Single Board Computer (SBC) Power Supply Unit (PSU) Solid State HD SATA (2x) AIR-Serial PROCESSADOR COMUNICAÇÃO Single Board Computer (SBC) Multiserial 8p Power Supply Unit (PSU) ET1 ET2 RS-xxx ET1 ET2 UP-A - Uplink Simplex (TELECOMANDO/Audio - Canal A) UP-B- Uplink Simplex (TELECOMANDO/Audio - Canal B) DOWN- Downlink Simplex (TELEMETRIA/Audio/Video - Canal único) PROCESSADOR DE COMUNICAÇÃO Back-UP (Futuro) Superf Comando - 10 Steering/Freio - 3 Motor - 4 CDB-B Single Board Computer (SBC) 2 x CAN Interface Power Supply Unit (PSU) SERIAL SERVER SWITCH-ET1 8 ports ET1 SWITCH-ET2 8 ports ET2 VIDEO PAN/CAUDA TELEMETRIA EAGLE TREE SERVOS Pots Temper PROCESSAMENTO DIGITAL ET1 ET2 1 2 2 3 4 5 6 7 8 RS-232 RS-232 RS-232 RS-232 RS-232 RS-xxx RS-xxx RS-xxx RS-xxx AHRS Back-up #1 AHRS Back-up #2 DISPARO PÁRA-QUEDAS BALÌSTICO MINI-BOOM INTERFACE (A) GPS RTK FALCÃO - C1 & C2 AVIÔNICOS Almir - 08/04/2010 AIR-Serial AIR-Serial AIR-Serial AIR-Serial AIR-Serial FALCÃO - SW ARCHITECTURE FALCÃO - AUTOPILOT FALCÃO - AIR - AVIONICS INTEGRATION RIG FALCÃO - AIR – SW INTEGRATION – 1ST CAMPAIGN FALCÃO - ENGINE 100 HP ROTAX 912 • 4 STROKES / 4 CILINDERS • 80 HP e 100 HP • WATER REFRIGERATION • REDUNDANT IGNITION • UNDER CERTIFICATION 80 HP FALCÃO – ENGINE TESTING FALCÃO - SYSTEM COMPOSITION Emprego Típico Reconnaissance Missions Air Defense Suppression Military Employment Communication Relay Reconnaissance Missions Artillery – Target Acquisition and Fire Correction COASTAL SURVEILLANCE Esolo 2 Esolo 1 BORDER SURVEILLANCE 1600 km CBRN SURVEILLANCE CP100 IMCell Module 90x130x60 mm Air Pump 60x60x60 mm Static Port URBAN SURVEILLANCE INTERNATIONAL EVENTS SECURITY Zona Amarela 25 min CCL 1 CCR 1 CCT 1 Zona Laranja 28 min CCL 2 CCR 2 CCT 2 Zona Vermelha 23 min CCL 3 Santos Dummont MARITIME SURVEILLANCE - PRÉ - SAL 80 nmi 150 km 15 nmi 28 km Zona ALFA - Circuito: 923 km - 5 h / ANV - 1,7 h / PO - Sincronização para Cobertura (TOT) SÃO PEDRO DA ALDEIA Zona BRAVO - Circuito: 1110 km - 6 h / ANV - 2 h / PO - Sincronização para Cobertura (TOT) ZONA BRAVO ZONA ALFA FALCÃO # 3 FALCÃO - MARITIME SURVEILLANCE FALCÃO - ARMED RECONNAISSANCE HARD POINTS • 4 points (Ribs #5 e #9) • Load Limit : 50 kg/point Guided Rocket Launchers Aux. POD´s External Underwing Fuel Tanks • Quant.: 2 un. • Quant.: 2 un. •Max. Mass: 50 kg • Capacity : 32 litres / each (25 kg) 70mm Guided Rockets • Quant.: 2 un. • Quant. Rockets : 03 / Launcher FALCÃO - ARMED RECONNAISSANCE Guided Rocket Launchers M9 70mm Guided Rockets M10 • Quant.: 2 un. • Quant. Rockets : 03 / Launcher GENERAL OVERVIEW – VANT SYSTEMS 2005 2006 2007 2008 2009 2010 2011 2012 Serial Production Project VANT – SNC - FINEP Military Missions 2013 Configuração de Missão / Certificação / Set-up Industrial VANT – FALCÃO - Avibras Auto Take-Off/Landing Civilian Missions Urban Surveillance, Public Security Data Link Tecnology Projects Motores FLIR Centrais Inerciais 2014 FALCÃO UAV SYSTEMS UAV SYSTEMS – OBJECTIVES Full autonomy and independence in key technologies: - Aeronautic structures made of Carbon Fiber composite material - Navigation, Control, Guidance and Auto-Pilot System - Integration of Full HD Electro optical Sensors - Integration of SAR/ISAR/GMTI Radars and E/O with SATCOM - Digital Secure Data and HD Imagery Communication - Software Post-Processing of Data and Imagery Information - Armed Configurations – Structural Hard Points on Wings - Spin off to Tactical Missiles - Technology => Autonomy => Political Independence SPIN OFF – TACTICAL MISILE SPIN OFF – TACTICAL MISILE MISSION PLANNIG AND SIMULATION SPIN OFF – TACTICAL MISILE Renato Tovar Gerente do Programa VANT AVIBRAS (12) 3955 6233 [email protected]
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