Tactical UAV System development activities started in 2007, first fully autonomous flight conducted in June 2009. With its unique composite airframe blended wing body design, system has advanced autonomy features with its high level hierachical flight control and guidance algorithms. Along with auto take off, automatic cruise modes and auto landing in high crosswind conditions, system can even handle the taxi phase autonomously. Wheel breaks are activated automatically as soon as the platform touchs down on the runway.
Specifications:
Wing Span: 9 m
Length: 5.5 m
Cruise Speed: 100 Knots
Endurance: 14 Hours
Flight Range: 1500 Km
Communication Range: 150 Km
Operational Altitude: 22,500 Feet
Autonomous Flight Features:
Automatic Taxi
Automatic Take Off
Automatic Flight
Automatic Landing
Cross Redundant Software & Architecture
Automatic Return Home & Landing in Case of Lost Comm
Flight Control System:
Automatic Guidance / Navigation
INS/GPS Navigation Capability
Kinematic Model Based Stochastic Filtering Algorithms
Automatic Landing Feature With Onboard Sensor Fusion Algorithms
Automatic Fuel Management Balancing Feature
Redundant Sensor Units (Pitot Static, GPS, IMU etc)
Fully Automatic Control From Taxi to Landing
Ground Control Station System (Cross Redundant Architecture)
Real Time Command / Control
Multi Display Feature
Pilot Console Unit
Copilot Console Unit
Ground Control Unit
Ground Data Terminal Unit
Automatic Tracking Antenna System
Flight Control System:
Automatic Guidance / Navigation
INS/GPS Navigation Capability
Kinematic Model Based Stochastic Filtering Algorithms
Automatic Landing Feature With Onboard Sensor Fusion Algorithms
Automatic Fuel Management Balancing Feature
Redundant Sensor Units (Pitot Static, GPS, IMU etc)
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