John Crassidis

PhD

John Crassidis.

John Crassidis

PhD

John Crassidis

PhD

Research Interests

Spacecraft attitude determination & control; formation flying guidance & navigation; robust nonlinear control; vehicle attitude dynamics

Contact Information

1003 Furnas Hall

Buffalo NY, 14260

Phone: (716) 645-1426

johnc@buffalo.edu

Biography Publications Teaching Research

Selected Publications

  • Wang, H., Chen, L., Jin, Z. and Crassidis, J.L., "Adaptive Momentum Distribution Jitter Control for a Micro-Satellite", Journal of Guidance, Control and Dynamics [Accepted]. https://arc.aiaa.org/doi/10.2514/1.G003909
  • Cheng, Y. and Crassidis, J.L., "A Total Least-Squares Estimate for Attitude Determination", 2019 AIAA Guidance, Navigation and Control Conference, AIAA SciTech Forum, San Diego, CA, Jan. 2019, AIAA Paper #2019-1176. https://arc.aiaa.org/doi/10.2514/6.2019-1176
  • Crassidis, J.L. and Cheng, Y., "Generalized Attitude Determination with One Dominant Vector Observation", Journal of Guidance, Control and Dynamics [Accepted]. https://arc.aiaa.org/doi/10.2514/1.G003717
  • Dianetti, A.D. and Crassidis, J.L., "Space Object Material Determination from Polarized Light Curves", 2019 AIAA Guidance, Navigation and Control Conference, AIAA SciTech Forum, San Diego, CA, Jan. 2019, AIAA Paper #2019-0377. https://arc.aiaa.org/doi/abs/10.2514/6.2019-0377
  • Schmid, M. and Crassidis, J.L. "A New Stochastic Control Paradigm Employing Large Deviations Theory," 2019 AIAA Guidance, Navigation and Control Conference, AIAA SciTech Forum, San Diego, CA, Jan. 2019, AIAA Paper #2019-2335. https://arc.aiaa.org/doi/abs/10.2514/6.2019-2335
  • Pimienta-Penalver, A. and Crassidis, J.L., "Estimating Attitude from Signal-to-Noise Ratio at Multiple Ground-Based Receivers", 2019 AIAA Guidance, Navigation and Control Conference, AIAA SciTech Forum, San Diego, CA, Jan. 2019, AIAA Paper #2019-0375. https://arc.aiaa.org/doi/abs/10.2514/6.2019-0375
  • Crassidis, J.L. and Cheng, Y., "Maximum Likelihood Analysis of the Total Least Squares Problem with Correlated Errors," 2019 AIAA Guidance, Navigation and Control Conference, AIAA SciTech Forum, San Diego, CA, Jan. 2019, AIAA Paper #2019-1931. https://arc.aiaa.org/doi/abs/10.2514/6.2019-1931
  • Ye, L., Zong, Q., Crassidis, J.L., and Tian, B., "Output Redefinition-Based Dynamic Inversion Control for a Nonminimum Phase Hypersonic Vehicle," IEEE Transactions on Industrial Electronics, vol. 65, no. 4, pp. 3447-3457, April 2018. https://ieeexplore.ieee.org/document/8061026
  • Dianetti, A.D., Weisman, R.M., and Crassidis, J.L., "Observability Analysis for Improved Space Object Characterization," Journal of Guidance, Control, and Dynamics, Vol. 41, No. 1, 2018, pp. 137-148. https://arc.aiaa.org/doi/10.2514/1.G002229
  • Linares, R. and Crassidis, J.L., "Space Object Shape Inversion via Adaptive Hamiltonian Markov Chain Monte Carlo," Journal of Guidance, Control, and Dynamics, Vol. 41, No. 1, 2018, pp. 47-58. https://arc.aiaa.org/doi/10.2514/1.G002296