• Research Works

  1. Development of hit-to-kill accurate guidance law for interceptor missiles using higher-order sliding mode control and optimal control.

  2. Development of high-wing single propeller fixed-wing nano aerial vehicle that fits inside a cube of 75 mm.

  3. Development of simultaneous stabilization based output feedback flight controllers for small aerial vehicles using robust control theory, eigenstructure assignment techniques, and genetic algorithm.

  4. Development of estimators for small aerial vehicles using robust estimation theory.

  5. Development of passive fault-tolerant flight controllers for unmanned combat aerial vehicle.