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

Actuators work in closed loop to counter external disturbances like wind

Reconfigurable robust inner loop flight control system.

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

Parallel hybrid systems allow an electric motor and IC Engine to power the drive train simultaneously

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

Follows desired trajectory despite external disturbances

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

Serial hybrid systems use an IC engine to turn an alternator and charge a battery using power electronic converters.

Prevents control saturation by redirecting control authority to other actuators

Fully inertial solution for attitude estimation

Prevents toppling of a multirotor even if it has just 3 working motors

Network centric platform for multiple opertors to manage multiple unmanned systems.

Greater maneuverability in Fixed wing and multirotors

Redirects actuator commands onto uncongested control bus

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

Vision based indoor localization

Underwater positioning system that acheives accuracy of LBL at a fraction of the cost.

Serves as a test bed for navigation and control law implementation

Use of multiple sensors with different characteristics for robust obstacle detection

Serves as a simulation and test bed for swarm control law implementations

Reliable low overhead secure asymmetric key encryption

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

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

Estimates mass of aircraft due to changes in payload/fuel

Efficient vector based motor control