Lee, T., Lee, B., & Sung, S. (2024, March). Invariant Kalman Filter Design for Securing Robust Performance of Magnetic–Inertial Integrated Navigation System under Measurement Uncertainty. Aerospace.
Chicago Style (17th ed.) CitationLee, Taehoon, Byungjin Lee, and Sangkyung Sung. "Invariant Kalman Filter Design for Securing Robust Performance of Magnetic–Inertial Integrated Navigation System Under Measurement Uncertainty." Aerospace Mar. 2024.
MLA (9th ed.) CitationLee, Taehoon, et al. "Invariant Kalman Filter Design for Securing Robust Performance of Magnetic–Inertial Integrated Navigation System Under Measurement Uncertainty." Aerospace, Mar. 2024.
Warning: These citations may not always be 100% accurate.
