1. Acquatella B., P., Falkena, W., van Kampen, E., and Chu, Q.P. (2012). Robust Nonlinear Spacecraft Attitude Control using Incremental Nonlinear Dynamic Inversion. In AIAA Guidance, Navigation, and Control Conference. American Institute of Aeronautics and Astronautics, Inc. (AIAA-2012-4623).
2. Acquatella B., P., van Kampen, E., and Chu, Q.P. (2013). Incremental Backstepping for Robust Nonlinear Flight Control. In EuroGNC 2013, 2nd CEAS Specialist Conference on Guidance, Navigation, and Control.
3. Bacon, B.J. and Ostroff, A.J. (2000). Reconfigurable Flight Control using Nonlinear Dynamic Inversion with a Special Accelerometer Implementation. In AIAA Guidance, Navigation, and Control Conference and Exhibit. (AIAA-2000-4565).
4. Bacon, B.J., Ostroff, A.J., and Joshi, S.M. (2000). Nonlinear Dynamic Inversion Reconfigurable Controller utilizing a Fault-tolerant Accelerometer Approach. Technical report, NASA Langley Research Center.
5. Recon-figurable NDI Controller using Inertial Sensor Failure Detection & Isolation;Bacon;IEEE Transactions on Aerospace and Electronic Systems,2001