This is my paper about complementary filter, UAV and navigation data fusion. Can be useful as example or template for creation of your own paper or Latex presentation.
This paper presents an analysis of complementary algorithm for inertial navigation systems. Proposed suboptimal algorithm for sensors data fusion of navigation system, this method employs combined complementary filter approach and attitude error equation of inertial navigation system. Simulation results are presented to demonstrate the performance of the proposed approach.