Attitude estimation on SO[3] based on direct inertial measurements

This publication has 4 references indexed in Scilit:

• Complementary filter design on the special orthogonal group SO(3)
  Published by Institute of Electrical and Electronics Engineers (IEEE) ,2006
• A coupled nonlinear spacecraft attitude controller and observer with an unknown constant gyro bias and gyro noise
  IEEE Transactions on Automatic Control, 2003
• Low-cost flight control system for a small autonomous helicopter
  Published by Institute of Electrical and Electronics Engineers (IEEE) ,2003
• Improving Control System Effectiveness for Ducted Fan VTOL UAVs Operating in Crosswinds
  Published by American Institute of Aeronautics and Astronautics (AIAA) ,2003