Y. Oshman and I. Y. Bar-Itzhack , “Eigenfactor Solution of the Matrix Riccati Equation—A Continuous Square Root Algorithm”, 23rd IEEE Conference on Decision and Control, Las Vegas, Nevada, Dec. 12–14, 1984.

Y. Oshman and I. Y. Bar-Itzhack , “New V-Lambda Square Root Filters”, 24th IEEE Conference on Decision and Control, Fort Lauderdale, Florida, December 11–13, 1985.

Y. Oshman and I. Y. Bar-Itzhack , “Square-Root Filtering via Covariance and Information Eigenfactors”, 28th Israel Annual Conference on Aviation and Astronautics, Tel-Aviv, Israel, February 1986.

Y. Oshman and I. Y. Bar-Itzhack , “Discrete-Time Gain-Free V-Lambda Filtering”, 25th IEEE Conference on Decision and Control, Athens, Greece, December 10–12, 1986.

Y. Oshman and D. J. Inman, “Square Root Filtering for Continuous-Time Models of Large Flexible Structures”, Sixth VPI&SU/AIAA Symposium on Dynamics and Control of Large Structures, Blacksburg, Virginia, June 29–July 1, 1987.

Y. Oshman and D. J. Inman, “Square-Root State Estimator for Large Space Structures”, Proc. of AIAA Guidance, Navigation and Control Conference, Monterey, California, August 17–19, 1987, pp. 617–627 (AIAA Paper No. 87-2389).

Y. Oshman and D. J. Inman, “Optimal On-Line Measurement System Configuration Strategies”, 29th AIAA Structures, Structural Dynamics and Materials Conference, Williamsburg, Virginia, April 18–20, 1988, pp. 1048–1049 (AIAA Paper No. 88-2341).

Y. Oshman , “Square-Root Information Filtering Using the Covariance Spectral Decomposition”, 27th IEEE Conference on Decision and Control, Austin, Texas, December 7–9, 1988, Vol. 1, pp. 382–387. Invited.

Y. Oshman , “On-Line Measurement Configuration Strategies for Discrete-Time Systems”, AIAA Guidance, Navigation and Control Conference, Minneapolis, Minnesota, August 15–17, 1988 (AIAA Paper No. 88-4168).

Y. Oshman , “Optimal Output Configuration Strategies for State Estimation in Large Space Structures”, IEEE International Conference on Control and Applications (ICCON), Jerusalem, Israel, April 3–6, 1989, pp. 819–824. Invited.

H. H. Cudney, D. J. Inman and Y. Oshman , “Distributed Structural Control Using Multilayered Piezoelectric Actuators-Analysis”, Seventh VPI&SU/AIAA Symposium on Dynamics and Control of Large Structures, Blacksburg, Virginia, May 8–10, 1989.

H. H. Cudney, D. J. Inman and Y. Oshman , “Distributed Actuators for Structural Control”, Proc. of American Control Conference, Pittsburgh, Pennsylvania, 21-23 June, 1989, pp. 1189–1194. Invited.

Y. Oshman , “Optimal Measurement Configuration for State Estimation”, AIAA Guidance, Navigation and Control Conference, Boston, Massachusetts, August 14–16, 1989 (AIAA Paper No. 89-3543).

H. H. Cudney, D. J. Inman and Y. Oshman , “Distributed Structural Control Using Multilayered Piezoelectric Actuators”, 31st AIAA Structures, Structural Dynamics and Materials Conference, Long Beach, California, April 2–4, 1990, pp. 2257–2265.

Y. Oshman , “Linear Quadratic Stochastic Control Using the Singular Value Decomposition”, AIAA Guidance, Navigation and Control Conference, Portland, Oregon, August 20–22, 1990 (AIAA Paper No. 90-3504).

Y. Oshman , “Maximum Likelihood State and Parameter Estimation Via Derivatives of the V-Lambda Filter”, AIAA Guidance, Navigation and Control Conference, New Orleans, Louisiana, August 12–14, 1991 (AIAA Paper No. 91-2772).

Y. Oshman , “A New, Factorized, Fixed-Interval Smoother”, AIAA Guidance, Navigation and Control Conference, Hilton Head, South Carolina, August 10–12, 1992 (AIAA Paper No. 92-4595).

T. Mendelboim, M. Bettoun, B. Englander, M. Gabel, Y. Oshman, “Drag/Thrust Estimation Via Aircraft Performance Flight Testing”, 18th Congress of the International Council of the Aeronautical Sciences, Beijing, People’s Republic of China, September 20–25, 1992 (Paper No. ICAS-92-2.7.1), pp. 1346–1354.

Y. Oshman and T. Mendelboim, “Maximum Likelihood Modal Parameter Identification and Realization of Stochastic Systems”, AIAA Guidance, Navigation and Control Conference, Monterey, California, August 9–11, 1993 (AIAA Paper No. 93-3840). **Best Paper in its Session.**

Y. Oshman and M. Isakow, “Decentralized Autonomous Attitude Determination Using An Inertially Stabilized Payload”, AIAA Guidance, Navigation and Control Conference, Monterey, California, August 9–11, 1993 (AIAA Paper No. 93-3854). **Best Paper in its Session**.

S. E. Miller, H. Abramovich and Y. Oshman , “Active Distributed Vibration Control of Laminated Composite Beams and Plates”, 4th International Conference on Adaptive Structures, Cologne, Germany, November 2–4, 1993.

S. E. Miller, H. Abramovich and Y. Oshman , “Active Distributed Vibration Control of General Anisotropic Piezo-Laminated Plates”, AIAA Guidance, Navigation and Control Conference, Scottsdale, Arizona, August 1–3, 1994 (AIAA Paper No. 94-3596).

S. E. Miller, Y. Oshman and H. Abramovich, “Distributed Modal Transducers for the Vibration Control of Anisotropic Composite Plates”, 45th International Astronautical Federation (IAF) Congress, Jerusalem, Israel, October 9–14, 1994 (Paper No. IAF-94-I.4.201).

S. E. Miller, Y. Oshman and H. Abramovich, “Selective Modal Control of Anisotropic Plates Via Selective Modal Transducers”, 36th AIAA Structures, Structural Dynamics and Materials Conference, New Orleans, Louisiana, April 10–12, 1995.

M. Ronen and Y. Oshman , “Minimal Parameter Solution of the Orthogonal Matrix Differential Equation Using the Peano-Baker Method”, AIAA Guidance, Navigation and Control Conference, Baltimore, Maryland, August 7–10, 1995 (AIAA Paper No. 95-3247).

S. E. Miller, Y. Oshman and H. Abramovich, “Selective Modal Vibration Control of Piezolaminated Shells Via Self-Sensing Selective Modal Actuators”, AIAA Guidance, Navigation and Control Conference, Baltimore, Maryland, August 7–10, 1995 (AIAA Paper No. 95-3255).

Y. Oshman and P. Davidson, “Optimal Observer Trajectories for Passive Target Localization Using Bearing-Only Measurements”, AIAA Guidance, Navigation and Control Conference, San Diego, California, July 29–31, 1996 (AIAA Paper No. 96-3740).

Y. Lipman, J. Shinar and Y. Oshman , “Analysis of Defense Scenarios Against Highly Maneuverable Anti-Surface Missiles”, 36th Israel Annual Conference on Aviation and Astronautics, Tel-Aviv and Haifa, Israel, February 21–22, 1996, pp. 246–257.

J. Shinar, Y. Lipman and Y. Oshman , “A Stochastic Analysis of the Interception of Maneuvering Anti-Surface Missiles”, AIAA Guidance, Navigation and Control Conference, San Diego, California, July 29–31, 1996 (AIAA Paper No. 96-3881).

S. E. Miller, H. Abramovich and Y. Oshman , “Experimental Validation of a Modal Transducer for an Orthotropic Rectangular Plate”, 38th AIAA Structures, Structural Dynamics and Materials Conference, Kissimmee, Florida, April 7–10, 1997 (AIAA Paper No. 97-1157).

Y. Oshman and F. L. Markley, “Efficient Sequential Attitude Estimation From Vector Observations”, Flight Mechanics Symposium, NASA Goddard Space Flight Center, Greenbelt, Maryland, May 19–21, 1997 (NASA Conference Publication 3345, pp. 331–345).

Y. Oshman and F. L. Markley, “Minimal-Parameter Attitude Matrix Estimation from Vector Observations”, AIAA Guidance, Navigation and Control Conference, New Orleans, Louisiana, August 11–13, 1997 (AIAA Paper No. 97-3451).

Y. Oshman and F. L. Markley, “Sequential Gyroless Attitude and Attitude-Rate Estimation from Vector Observations”, 48th International Astronautical Federation (IAF) Congress, Turin, Italy, October 6–10, 1997 (Paper No. IAF-97-A.2.07). **Best Paper in its Session**.

S. E. Miller, Y. Oshman and H. Abramovich, “Selective Modal Control of Composite Piezolaminated Anisotropic Shells”, SPIE Smart Structures and Materials 1998: Mathematics and Control in Smart Structures, San Diego, California, March 1–6, 1998 (Proceedings of SPIE, Vol. 3323, Paper No. 3323-24).

S. E. Miller, Y. Oshman and H. Abramovich, “Modal Transducers for Piezolaminated Anisotropic Zero-Gaussian Curvature Shell Systems”, 39th AIAA Structures, Structural Dynamics and Materials Conference, Long Beach, California, April 20–23, 1998 (AIAA Paper No. 98-1953).

Y. Oshman and F. L. Markley, “Attitude/Attitude-Rate Estimation From GPS Differential Phase Measurements Using Integrated-Rate Parameters”, AAS/GSFC 13th International Symposium on Space Flight Dynamics, NASA Goddard Space Flight Center, Greenbelt, Maryland, May 11–15, 1998, AAS Paper No. 98-329, NASA CP-1998-206858 Vol. I, pp. 311–325.

Y. Oshman and F. L. Markley, “Sequential Gyroless Attitude/Attitude-Rate Estimation Using Integrated-Rate Parameters”, AIAA Guidance, Navigation and Control Conference, Boston, Massachusetts, August 10–12, 1998 (AIAA Paper No. 98-4508).

Y. Oshman , J. Shinar and S. Avrashi Weizman, “Using a Multiple Model Adaptive Estimator in a Random Evasion Missile/Aircraft Encounter”, AIAA Guidance, Navigation and Control Conference, Portland, Oregon, August 9–11, 1999 (AIAA Paper No. 99-4141).

Y. Oshman and F. Dellus, “Spacecraft Angular Velocity Estimation Using Sequential Observations of a Single Vector”, AAS/AIAA Astrodynamics Specialist Conference, Girdwood, Alaska, August 16–18, 1999, AAS Paper No. AAS 99-426.

Y. Oshman and F. Dellus, “Spacecraft Angular Rate Estimation from a Single Directional Vector”, 50th International Astronautical Federation (IAF) Congress, Amsterdam, The Netherlands, October 4–8, 1999 (Paper No. IAF-99-A.3.02). **Best Paper in its Session**.

Y. Oshman and F. Dellus, “Fast Estimation of Spacecraft Angular Velocity from Sequential Geomagnetic Field Observations”, AAS/AIAA Astrodynamics Specialist Conference, Denver, Colorado, August 14–17, 2000 (AIAA Paper No. AIAA 2000-4242).

P. Tortora and Y. Oshman , “Spacecraft Angular Rate Estimation from Magnetometer Data Only”, AAS/AIAA Astrodynamics Specialist Conference, Denver, Colorado, August 14–17, 2000 (AIAA Paper No. AIAA 2000-4240, pp. 304–310).

J. Alkahe, O. Rand and Y. Oshman , “Damage Detection in a Rotating Helicopter Blade Using an Adaptive Estimator”, AIAA Guidance, Navigation and Control Conference, Denver, Colorado, August 14–17, 2000 (AIAA Paper No. AIAA 2000-4569).

Y. Oshman and I. Shaviv, “Optimal Tuning of a Kalman Filter Using Genetic Algorithms”, AIAA Guidance, Navigation and Control Conference, Denver, Colorado, August 14–17, 2000 (AIAA Paper No. AIAA 2000-4558).

T. Shima, Y. Oshman and J. Shinar, “An Efficient Application of Multiple Model Adaptive Estimation in Ballistic Missile Interception Scenarios”, AIAA Guidance, Navigation and Control Conference, Denver, Colorado, August 14–17, 2000 (AIAA Paper No. AIAA 2000-4274).

J. Alkahe, O. Rand and Y. Oshman , “Damage Detection in a Helicopter Rotor by Adaptive Estimation”, 26th European Rotorcraft Forum, 26–29 September 2000, The Hague, The Netherlands, pp. 85.1–85.8.

J. Alkahe, O. Rand and Y. Oshman , “Helicopter Rotor Health Monitoring Using Adaptive Estimation”, Proc. of AHS—International Forum 57, Washington, DC, May 9–11, 2001.

Y. Oshman and D. Arad, “Using Target Orientation To Enhance Air-to-Air Missile Target Tracking”, Proc. of Workshop on Estimation, Tracking and Fusion: A Tribute to Yaakov Bar-Shalom, Naval Postgraduate School, Monterey, CA, May 17, 2001, pp. 496–512. Invited.

Y. Oshman and D. Arad, “Enhanced Air-to-Air Missile Tracking Using Target Orientation Observations“, AIAA Guidance, Navigation and Control Conference, Montreal, Canada, August 6–9, 2001 (AIAA Paper No. AIAA 2001-4110).

Y. Oshman , A. Rubanenko and H. Rotstein, “State Estimation Using Measurements With Uncertain Time-Tag”, AIAA Guidance, Navigation and Control Conference, Montreal, Canada, August 6–9, 2001 (AIAA Paper No. AIAA 2001-4399).

D. Choukroun, I. Y. Bar-Itzhack and Y. Oshman , “Optimal REQUEST Algorithm for Attitude Determination”, AIAA Guidance, Navigation and Control Conference, Montreal, Canada, August 6–9, 2001 (AIAA Paper No. AIAA 2001-4153).

Y. Oshman and D. Arad, “A New Differential-Game Based Guidance Law Using Target Orientation Observations“, AIAA Guidance, Navigation and Control Conference, Monterey, CA, August 5–8, 2002 (AIAA Paper No. AIAA 2002-3828).

M. Almogi-Nadler, Y. Oshman and J. Z. Ben-Asher, “Boost-Phase Identification of Theatre Ballistic Missiles Using Radar Measurements”, AIAA Guidance, Navigation and Control Conference, Monterey, CA, August 5–8, 2002 (AIAA Paper No. AIAA 2002-3893).

D. Choukroun, I. Y. Bar-Itzhack and Y. Oshman , “A Novel Quaternion Kalman Filter”, AIAA Guidance, Navigation and Control Conference, Monterey, CA, August 5–8, 2002 (AIAA Paper No. AIAA 2002-3902).

M. L. Psiaki and Y. Oshman , “Spacecraft Attitude Rate Estimation from Geomagnetic Field Measurements”, AIAA Astrodynamics Specialist Conference, Monterey, CA, August 5–8, 2002 (AIAA Paper No. AIAA 2002-4828). **Selected as Best Paper of this Conference**.

I. Rapoport and Y. Oshman , “Optimal Filtering in the Presence of Faulty Measurement Biases”, 2002 IEEE Conference on Decision and Control (CDC’02), Las Vegas, Nevada, December 10–13, 2002.

I. Rapoport and Y. Oshman , “Fault Adaptive Filtering and its Application to Spacecraft Attitude Estimation”, Proc. 43rd Israel Annual Conference on Aerospace Sciences, Tel-Aviv and Haifa, Israel, February 19–20, 2003.

P. Tortora, Y. Oshman and F. Santoni, “Attitude Independent Estimation of Spacecraft Angular Rate Using Geomagnetic Field Observations”, 2003 IEEE Aerospace Conference, Big Sky, MT, March 8-15, 2003 (Paper No. 1420).

Y. Zimmerman, A. Brandes and Y. Oshman , “New Analog Encoder Filtering Algorithm Based on EKF”, 2003 Mechanical Engineering Conference, Haifa, Israel, May 12–13, 2003.

J. Shinar, Y. Oshman , V. Turetsky and J. Evers, “On the Need for Integrated Estimation/Guidance Design for Hit-to-kill Accuracy”, 2003 American Control Conference, Denver, Colorado, June 4–6, 2003, pp. 402–407.

Y. Zimmerman, A. Brandes and Y. Oshman , “Improving the Accuracy of Analog Encoders Via Kalman Filtering”, 5th IFAC International Symposium on Intelligent Components and Instruments for Control Applications (SICICA-2003), Aveiro, Portugal, July 9–11, 2003.

R. Harman, J. Thienel and Y. Oshman , “Testing of Gyroless Estimation Algorithms for the FUSE Spacecraft”, AIAA Astrodynamics Specialist Conference, Big Sky, Montana, August 3–7, 2003 (Paper No. AAS 03-605).

Y. Oshman and M. Koifman, “Robust GPS Navigation in the Presence of Jamming and Spoofing”, AIAA Guidance, Navigation and Control Conference, Austin, TX, August 11–14, 2003 (AIAA Paper No. AIAA 2003-5668). **Best Paper in its Session**.

D. Choukroun, H. Weiss, I. Y. Bar-Itzhack and Y. Oshman , “Attitude Matrix Estimation from Vector Observations Using a Matrix Kalman Filter”, AIAA Guidance, Navigation and Control Conference, Austin, TX, August 11–14, 2003 (AIAA Paper No. AIAA 2003-5482).

R. Harman, J. Thienel and Y. Oshman, “Gyroless Attitude and Rate Estimation Algorithms for the FUSE Spacecraft”, Flight Mechanics Symposium, NASA Goddard Space Flight Center, Greenbelt, Maryland, October 28-30, 2003.

I. Rapoport and Y. Oshman , “A New Estimation Lower Bound for Interruption Indicators in Systems with Uncertain Measurements”, Proceedings of IEEE 2003 Conference on Decision and Control (CDC’03), Maui, Hawaii, December 9–12, 2003.

I. Rapoport and Y. Oshman , “A Cramér-Rao Type Lower Bound for the Estimation Error of Systems with Measurement Faults”, Proceedings of IEEE 2003 Conference on Decision and Control (CDC’03), Maui, Hawaii, December 9–12, 2003.

D. Choukroun, H. Weiss, I. Y. Bar-Itzhack and Y. Oshman , “State Matrix Kalman Filter”, Proceedings of IEEE 2003 Conference on Decision and Control (CDC’03), Maui, Hawaii, December 9–12, 2003.

Y. Oshman and A. Carmi, “Spacecraft Attitude Estimation from Vector Observations Using a Fast Particle Filter”, Proceedings of 14th AAS/AIAA Space Flight Mechanics Conference, Maui, Hawaii, February 8–12, 2004 (Paper No. AAS 04-141).

D. Dionne, H. Michalska and Y. Oshman , “Terminal Missile Guidance Using a Semi-Markov Target Model”, Proceedings of 16th IFAC Symposium on Automatic Control in Aerospace, St. Petersburg, Russia, June 14–18, 2004. Invited.

Y. Oshman and A. Carmi, “Estimating Attitude from Vector Observations Using a Genetic Algorithm-Embedded Quaternion Particle Filter”, AIAA Guidance, Navigation and Control Conference, Providence, Rhode Island, August 16–19, 2004 (Paper No. AIAA-2004-5340). **Selected as Best Paper of this Conference**.

I. Rapoport and Y. Oshman , “Fault Tolerant Particle Filtering Using IMM-Based Rao-Blackwellization”, AIAA Guidance, Navigation and Control Conference, Providence, Rhode Island, August 16–19, 2004 (Paper No. AIAA-2004-5416).

I. Rapoport and Y. Oshman , “Efficient Fault Tolerant Estimation Using the IMM Methodology”, AIAA Guidance, Navigation and Control Conference, Providence, Rhode Island, August 16–19, 2004 (Paper No. AIAA-2004-5417).

Y. Oshman and M. Koifman, “Robust, IMM-Based, Tightly-Coupled INS/GPS in the Presence of Spoofing”, AIAA Guidance, Navigation and Control Conference, Providence, Rhode Island, August 16–19, 2004 (Paper No. AIAA 2004-4776).

J. Shinar, V. Turetsky and Y. Oshman , “New Logic Based Estimation/guidance Algorithm for Improved Homing Against Randomly Maneuvering Targets”, AIAA Guidance, Navigation and Control Conference, Providence, Rhode Island, August 16–19, 2004 (Paper No. AIAA 2004-5417).

J. Evers, J. Shinar, Y. Oshman and V. Turetsky, “Integrated Estimator/Guidance Law Design for Improved Ballistic Missile Defense”, AIAA Missile Sciences Conference, Monterey, CA, November 16–18, 2004.

I. Rapoport and Y. Oshman , “Recursive Weiss-Weinstein Lower Bounds for Discrete-Time Nonlinear Filtering”, 43rd IEEE Conference on Decision and Control (CDC’04), Paradise Island, The Bahamas, December 14–17, 2004.

A. Carmi and Y. Oshman, “Robust Spacecraft Angular-Rate Estimation from Vector Observations Using Fast Interlaced Particle Filtering”, AIAA Guidance, Navigation and Control Conference, San Francisco, California, August 15-18, 2005 (Paper No. AIAA-2005-6399).

D. Choukroun, H. Weiss, I. Y. Bar-Itzhack and Y. Oshman, “Quaternion Estimation from Vector Observations Using a Matrix Kalman Filter”, AIAA Guidance, Navigation and Control Conference, San Francisco, California, August 15-18, 2005 (Paper No. AIAA-2005-6397).

I. G. Shaviv and Y. Oshman, “Guidance Without Assuming Separation”, AIAA Guidance, Navigation and Control Conference, San Francisco, California, August 15-18, 2005 (Paper No. AIAA-2005-6154).

I. G. Shaviv and Y. Oshman, “Fusion of Estimation and Guidance Using Sequential Monte Carlo Methods”, Proceedings of IEEE Conference on Control Applications, Toronto, Canada, August 28-31, 2005, pp. 1361-1366. Invited.

A. Carmi and Y. Oshman, “Vector Observations-Based Gyroless Spacecraft Attitude/Angular Rate Estimation Using Particle Filtering”, AIAA Guidance, Navigation and Control Conference, Keystone, Colorado, August 21-24, 2006 (Paper No. AIAA-2006-6597).

I. G. Shaviv and Y. Oshman, “Estimation-Guided Guidance”, AIAA Guidance, Navigation and Control Conference, Keystone, Colorado, August 21-24, 2006. Invited. (Paper No. AIAA-2006-6217).

Y. Cheng, F. L. Markley, J. L. Crassidis, and Y. Oshman, “Averaging Quaternions”, AAS/AIAA *Space Flight Mechanics Meeting*, Sedona, Arizona, January 28 – February 1, 2007.

M. Goldshtein, Y. Oshman, T. Efrati, “Computer Vision-Based Compensation of Gyro Bias and Scale-Factor Errors,” 10th International Conference on Information Fusion (FUSION 2007), Quebec City, Canada, July 9-12, 2007.

A. Carmi and Y. Oshman, “On the Covariance Singularity of Quaternion Estimators”, AIAA Guidance, Navigation and Control Conference, Hilton Head, South Carolina, August 20-23, 2007 (Paper No. AIAA-2007-6814).

A. Carmi and Y. Oshman, “On the Observability of the Spacecraft Attitude and Angular Rate Estimation Problem”, AAS F. Landis Markley Astronautics Symposium, Cambridge, Maryland, June 29-July 2, 2008.

M. Goldshtein, Y. Oshman, and T. Efrati, “Seeker Gyro Calibration Via Model-Based Fusion of Visual and Inertial Data, AIAA Guidance, Navigation and Control Conference, Honolulu, Hawaii, August 18-21, 2008.(Paper No. AIAA 2008-7424).

V. Shaferman and Y. Oshman, “Cooperative Interception in a Multi-Missile Engagement”, AIAA *Guidance, Navigation and Control Conference*, Chicago, IL, August 10-13, 2009. (Paper No. AIAA 2009-5783).

D. Sigalov and Y. Oshman, “State Estimation in Hybrid Systems With a Bounded Number of Mode Transitions”, *13th International Conference on Information Fusion (FUSION 2010)*, Edinburgh, United Kingdom, 26-29 July 2010.

D. Sigalov and Y. Oshman, “A New Formulation of Fault-Tolerant Estimation Problems and Some Solutions”, 2010 IEEE *26th Convention of Electrical and Electronics Engineers in Israel (IEEEI 2010),* Eilat, Israel, 17-19 November, 2010.

D. Sigalov and Y. Oshman, “Linear Optimal Estimation Problems in Systems with Actuator Faults”, *14th International Conference on Information Fusion (FUSION 2011)*, Chicago, IL, July 5-8, 2011.

D. Sigalov and Y. Oshman, “Tracking Maneuvering Targets with a Soft Bound on the Number of Maneuvers”, *14th International Conference on Information Fusion (FUSION 2011)*, Chicago, IL, July 5-8, 2011.

S. Vichik and Y. Oshman, “Optimal Covariance Selection for Estimation Using Graphical Models”, *American Control Conference (ACC 2011)*, San Francisco, CA, June 29 — July 1, 2011.

D. Sigalov and Y. Oshman, “Linear Optimal State Estimation in Systems with Independent Mode Transitions”, *50th IEEE Conference on Decision and Control,* Orlando, FL, December 12-15, 2011.

D. Sigalov, N. Leiter, N. Kalish, Y. Oshman, “State Estimation in Hybrid Systems with a Bounded Number of Mode Transitions in the Presence of Spurious Measurements”, *15th International Conference on Information Fusion (FUSION 2012)*, Singapore, July 9-12, 2012.

D. Sigalov, T. Michaeli, Y. Oshman, “Unified Approach to State Estimation Problems Under Data and Model Uncertainties”, *15th International Conference on Information Fusion (FUSION 2012)*, Singapore, July 9-12, 2012.

D. Sigalov, T. Michaeli, Y. Oshman, “Tracking a Splitting Target in Clutter Using the IMM Methodology”, *27th Convention of Electrical and Electronics Engineers in Israel (IEEEI 2012)*, Eilat, Israel, November 14-17, 2012. **Best student paper of this conference**.

D. Sigalov and Y. Oshman, “Modeling Maneuvering Targets with GARCH”, *53rd Israel Annual Conference on Aerospace Sciences*, Tel-Aviv and Haifa, Israel, March 6-7, 2013.

A. J. Friedman, Y. Oshman, J. Cohen, “System Order and Sensing Resolution Reduction for Subcritical Incompressible Plane Poiseuille Flow State Estimation”, *53rd Israel Annual Conference on Aerospace Sciences*, Tel-Aviv and Haifa, Israel, March 6–7, 2013.

D. Sigalov, T. Michaeli, Y. Oshman, “Tracking an Extended Maneuvering Target Using a Novel Modeling of Systems with Random Parameters”, *54th Israel Annual Conference on Aerospace*

* Sciences*, Tel-Aviv and Haifa, Israel, February 19-20, 2014.

A. J. Friedman, Y. Oshman, J. Cohen, “Balanced Truncation of System Models Using Reduced Resolution Sensing for Plane Poiseuille Flow State Estimation”, *7th AIAA Flow Control **Conference*, Atlanta, Georgia, 16-20 June, 2014 (within AVIATION 2014).

D. Sigalov, T. Michaeli, Y. Oshman, “Simultaneous Tracking and Data Association in an Extended Maneuvering Target Using the IMM Methodology”, *17th International Conference on Information **Fusion (FUSION 2014)*, Salamanca, Spain, 7-10 July, 2014.

D. Sigalov and Y. Oshman, “On a Possible Division by Zero in the Interacting Multiple Model (IMM) Filter”, *28th **Convention of Electrical and Electronics Engineers in Israel **(IEEEI 2014)*, Eilat, Israel, December 3-5, 2014.

A. J. Friedman, Y. Oshman, J. Cohen, “Transition Thresholds for Plane Poiseuille Flow Using Selective Wave-Number Pair Control”, *55th Israel Annual Conference on Aerospace **Sciences*, Tel-Aviv and Haifa, Israel, February 25-26, 2015.

D. Sigalov and Y. Oshman, “A Novel Method for GPS Navigation in the Presence of Spoofing”, *55th Israel Annual Conference on Aerospace Sciences*, Tel-Aviv and Haifa, Israel, February 25-26, 2015.