top of page
2726243.jpg

Technologies

 Tightly Coupled INS-GPS UKF

Unscented Kalman filter for position, velocity, attitude estimation that works even in partially GPS denied environments.

All Unmanned Vehicles (Air/Land)

➤ Teragrid

Vision based indoor localization

Indoor mobile robots primarily for warehouse navigation

➤ Attitude Heading Reference System (AHRS)

Fully inertial solution for attitude estimation

All unmanned vehicles and alignment systems

➤ Aerodata Estimation From Flight Tests

Determine Aerodynamic data of Fixed wing planes from flight tests of a scaled model

Eliminates need for wind tunnel tests

 Synthetic Air Data System

Unscented Kalman filter to estimate Angle of attack and sideslip from inertial sensors and aerodatabase

Auxillary stand by sensor for large aircraft or stand alone system for small aircraft

 Radar Camera Fusion

Use of multiple sensors with different characteristics to provide a comprehemsive picture of the surroundings

All Unmanned Systems

 Radar Camera Fusion

Estimates mass of aircraft due to changes in payload/fuel

All aerial sytems

 Quatos Robust Adaptive Attitude Controller

Reconfigurable flight control system

Allows the craft to fly in severe external disturbances and actuator failure

 Adaptive Thrust Control

Actuators work in closed loop to counter external disturbances like wind

All VTOL systems

➤ Control Redundancy

In case one flight controller fails, another takes over and so on...

All large unmanned systems

➤ Control Bus Redundancy

Redirects commands onto uncongested control bus

Large systems

➤ Hardware In Loop Simulator (HILS)

Serves as a test bed for navigation and control law implementation

All manned/unmanned systems

➤ Swarm Simulator

Serves as a test bed for swarm control law implementations

All unmanned systems

 Stardust

Network centric platform for multiple opertors to manage multiple unmanned systems

All large vehicle/drone fleets

 Paradox Encryption

Reliable low overhead secure Asymmetric key communications

All communication systems

 Hybrid Power Systems

Using an alternator to recharge a battery pack

Auxillary power systems for aircraft

 Active Battery Management Systems

Automatic efficient cell balancing

All electric vehicles

 Direct Drive Systems

Serial and parallel hybrid drive chains

Hybrid vehicles

 Dynamic Control Allocation

Prevents control saturation by redirecting control authority to other actuators

All unmanned systems

➤ Yaw Decoupling

Prevents toppling of a multirotor with just 3 working motors

All multirotors

➤ Adaptive Navigation Controller

Follows desired trajectory despite external disturbances

All Aerial/aquatic systems

➤ Activ Avoidance

Allows care free automated flight amidst obstacles that are user designated or detected using a suitable vision based system

All VTOL systems

 Analytical gain tuning for nonlinear flight control laws

Theoretically proven and derivable control law tuning, necessary for certification of large craft

Aerial systems

 Thrust Vectoring

Greater maneuverability in Fixed wing and multirotors

Aerial systems

 Actuator Feedback

Incorporating feedback of actuator position into control law provides a larger phase margin for stability

Improved tracking performance in Aerial/ Aquatic systems

 Field Oriented Control

Efficient motor control

All PMSM/BLDC motors

bottom of page