Professional Experience

Education

PhD, Aerospace Engineering, Virginia Polytechnic Institute and State University, 1998

MS, Aeronautics and Astronautics, Purdue University, 1993

BS, Aerospace Engineering ( Magna Cum Laude), West Virginia University, 1991

Professional Activities

Associate Editor, AIAA Journal of Guidance, Control and Dynamics

Associate Editor, IEEE Control Systems Society Conference Editorial Board

Associate Member, AIAA Technical Committee on Guidance Navigation and Control

Associate Fellow, American Institute of Aeronautics and Astronautics (AIAA)

Senior Member, IEEE

Publications

Oppenheimer, M.W. and Doman, D.B., “Methods for Compensating for Control Allocator and Actuator Interactions”, Journal of Guidance, Control and Dynamics, Vol. 27, No. 5, Sept-Oct, 2004.

Bolender, M. A. and Doman, D.B., “A Method for the Determination of Attainable Moment Sets for a Class of Non-Linear Control Effectors”. Journal of Guidance, Control and Dynamics, Vol 27, No. 5, Sept-Oct, 2004

Schierman, J.D., Ward D.G., Hull, J.R., Gandhi, N., Oppenheimer, M.W. and Doman, D.B., “An Approach to Integrated Adaptive Guidance and Control with Flight Test Results”, to appear in Journal of Guidance, Control and Dynamics, Vol. 27, No. 6, November-December, 2004

Bolender, M. A. and Doman, D.B., “Non-linear Control Allocation Using Piecewise Linear Functions”. scheduled to appear in Journal of Guidance, Control and Dynamics, Vol 27, No. 6, Nov-Dec, 2004

Mitchell, D., Schmidt, D.K., Doman, D.B., et. al. “The Evolution and Revolution of Handling Qualities”, Journal of Guidance Control and Dynamics, Jan-Feb, Vol. 27, No. 1, 2004.

Iyer, R.V., Holsapple, R. and Doman D.B., “Optimal Control Problems on Parallelizable Riemannian manifolds: Theory and Applications”, ESAIM: Control, Optimisation and Calculus of Variations, to appear.

Doman, D.B. and Oppenheimer, M.W., “Integrated Adaptive Guidance and Control for Space Access Vehicles, Vol. I Reconfigurable Control Law for X-40A Approach and Landing” , AFRL-VA-WP-TR-2004-3075, Technical Report

Scheirman, J.D., Ward D.G., Hull, J.R., Gandhi, N., Oppenheimer, M.W. and Doman, D.B., “Integrated Adaptive Guidance and Control for Space Access Vehicles, Vol II Trajectory Reshaping and Adaptive Guidance for X-40A” AFRL-VA-WP-TR-2004-3076, Technical Report

Holsapple, R., Venkataraman, R. and Doman, D.B.,“A New, Fast Numerical Method for Solving Two Point Boundary Value Problems”, Journal of Guidance, Control and Dynamics, Vol. 27, No. 2, 2004.

Fahroo, F. and Doman,D.B., “A Direct Method for Approach and Landing Trajectory Reshaping with Failure Effect Estimation”, in Proceedings of 2004 AIAA Guidance, Navigation and Control Conference.

Shankar, P., Yedavalli, R.K. and Doman, D.B., “Stability Domain Calculation of a Dynamic Inversion Based State Dependent Riccatti Equation Controller for a Flight Vehicle”, in Proceedings of 2004 AIAA Guidance, Navigation and Control Conference.

Bolender, M.A., and Doman, D.B., “Nonlinear Control Allocation using Piecewise Linear Functions, A Linear Programming Approach”, in Proceedings of 2004 AIAA Guidance, Navigation and Control Conference.

Oppenheimer, M.W., Doman, D.B. and Bolender M.A. , “A Method for Estimating Control Failure Effects for Aerodynamic Vehicle Trajectory Retargeting”, ”, in Proceedings of 2004 AIAA Guidance, Navigation and Control Conference.

Oppenheimer, M.W. and Doman, D.B.,” Reconfigurable Control Design for the X-40A with In-Flight Simulation Results”, ”, in Proceedings of 2004 AIAA Guidance, Navigation and Control Conference.

Venkataraman, R., Oppenheimer, M.W. and Doman, D.B., “A New Control Allocation Algorithm that Accounts for Effector Dynamics”, Proceedings of 2004 IEEE Aerospace Conference.

Trent, A., Venkataraman, R., and Doman, D.B., “Trajectory Generation Using a Modified Simple Shooting Method”, Proceedings of the 2004 IEEE Aerospace Conference.

Luo, Y., Yurkovich S., Serrani A., Doman D.B. and Oppenheimer M.W., “Model Predictive Dynamic Control Allocation with Actuator Dynamics”, in Proceedings of 2004 American Control Conference.

Poonamalee, V., Yurkovich S., Doman D.B. and Oppenheimer, M.W., “A Nonlinear Programming Approach for Control Allocation”, in Proceedings of 2004 American Control Conference.

Doman, D.B. and Oppenheimer, M.W., “Adaptive Guidance and Control for Space Operating Vehicles”, in Proceedings of the 2003 Joint Army, Navy, NASA, Air Force (JANNAF) Interagency Propulsion Committee Meeting.

Oppenheimer, M.W. and Doman, D.B.,“Adaptive Guidance, Navigation and Control for Space Operating Vehicles”, in Proceedings of 2003 CORE Technologies for Space Systems Conference.

Mitchell, D., Schmidt, D.K., Doman, D.B., et. al. “The Evolution and Revolution of Handling Qualities”. In proceedings of 2003 AIAA Atmosheric Flight Mechanics Conference, AIAA Paper 2003-5465

Bolender, M. A. and Doman, D.B., “Non-linear Control Allocation Using Piecewise Linear Functions”. in Proceedings of 2003 AIAA Guidance Navigation and Control Conference, AIAA Paper 2003-5357

Oppenheimer, M.W. and Doman, D.B.,“Reconfigurable Inner Loop Control for the X-40A Space Maneuvering Vehicle”, in Proceedings of 2003 AIAA Guidance Navigation and Control Conference, AIAA Paper 2003-5358

Shankar, P. Yedavalli, R.K. and Doman, D.B.,“Dynamic Inversion via State Dependent Riccati Equation Approach: Application to Hypersonic Vehicles”, In Proceedings of 2003 AIAA Guidance Navigation and Control Conference, AIAA Paper 2003-5361

Fahroo, F., Doman D.B., and Ngo, A.D., “Footprint Generation for Reusable Launch Vehicles Using a Direct Pseudo-Spectral Method”. in Proceedings of the 2003 American Control Conference ACC03-AIAA0007.

Shankar, P., Yedavalli, R.K. and Doman, D.B., “Robustness Study of the Dynamic Inversion Based Indirect Adaptive Control of Flight Vehicles with Uncertain Model Data”, in Proceedings of the 2003 American Control Conference.

Doman, D.B. and Kaloust, J., “An Algorithm for Computing the Range of Trimmable Angle of Attack for Aircraft Experiencing Control Effector Failures”, in Proceedings of 2003 IEEE Aerospace Conference.

Holsapple, R., Venkataraman, R. and Doman, D.B.,“A Modified Simple Shooting Method for Two Point Boundary Value Problems”, in Proceedings 2003 IEEE Aerospace Conference.

Bolender, M.A. and Doman, D.B., “A Method for the Determination of the Attainable Moment Set for Nonlinear Control Effectors”, in Proceedings of 2003 IEEE Aerospace Conference.

Fahroo, F., Doman D.B. and Ngo, A.D., “A New Approach to Real-Time Footprint Generation for Hypersonic Vehicles”, in Proceedings of 2003 IEEE Aerospace Conference.

Doman, D.B. and Oppenheimer, M.W., “Improving Control Allocation Accuracy for Nonlinear Aircraft Dynamics”, in Proceedings of the 2002 AIAA Guidance Navigation and Control Conference, AIAA Paper 2002-4667

Ngo, A.D., and Doman, D.B.,“Footprint Determination for Reusable Launch Vehicles Experiencing Control Effector Failures ”, invited paper, in Proceedings of the 2002 AIAA Guidance Navigation and Control Conference, AIAA Paper 2002-4775

Doman, D.B. and Sparks, A.G., “Concepts for Constrained Control Allocation of Mixed Quadratic and Linear Effectors”, American Control Conference (ACC), Anchorage, AK, May, 2002.

Ngo, A.D., and Doman, D.B.,“Footprint Calculation Methods for a Reusable Launch Vehicle”, American Control Conference (ACC), Anchorage, AK, May, 2002.

Doman, D.B., Ngo, A. D., "Dynamic Inversion-Based Adaptive/Reconfigurable Control of the X-33 on Ascent" , AIAA Journal of Guidance Control and Dynamics, Vol 25, No. 2, pp. 275-284.

Ngo, A. D., Doman D.B, ``Techniques to Improve the Regressor Matrix Condition for Real-Time Parameter Identification,’’ ACC01-SHT1062, American Control Conference (ACC), Crystal City, Virginia, June 2001

Venkataraman, Ram and Doman, D.B., “Control Allocation and Compensation for Over-Actuated Systems with Non-Linear Effectors” ACC01-SHT1-72, American Control Conference (ACC), Crystal City, Virginia, June 2001

Doman, D. B. and Ngo, A. D., “Dynamic Inversion-Based Adaptive Reconfigurable Control of the X-33 on Ascent”, Proceedings of the IEEE Aerospace Conference, Big Sky MT, Mar, 2001.

Doman, D.B., Leggett D.B., Saliers M.A., and Pachter, Meir, “Development of a Hybrid Direct/Indirect Adaptive Control System for the X-33”, Invited Paper, AIAA Guidance Navigation and Control Conference, Denver CO, Aug 2000, AIAA Paper 2000-4156

Naidu, D.S., Doman, D.B. and Banda, S.S., “Sky print for X-33 vehicle via neighboring optimal control.”, American Control Conference (ACC), Chicago, IL, June 2000.

Doman, D.B. and Anderson, M.R., A fixed-order optimal control model of human operator response, Automatica, 36 (3), March 2000 pp. 409-418.

Doman, David B. , “Optimal control pilot modeling for resolving Cooper-Harper rating discrepancies.”, AIAA Atmospheric Flight Mechanics Conference and Exhibit, Portland, OR, Aug. 9-11, 1999; p. 176-186, AIAA Paper 99-4091

Doman, David B. , “On the feasibility of piloting hypersonic vehicles - A pilot modeling approach.”, AIAA Paper 99-4127, Invited Paper, AIAA Guidance, Navigation, and Control Conference and Exhibit, Portland, OR, Aug. 9-11, 1999; p. 892-900, AIAA Paper 99-4127.

Doman, D.B. and Anderson, M.R., “Minimal Representations of Human Operator Dynamics in Compensatory Systems.” In Proceedings of AIAA Guidance, Navigation and Control Conference, Boston, MA, August 1998, AIAA Paper 98-4143

Doman, D.B., “Projection Methods For Order Reduction of Optimal Human Operator Models”. Ph.D. Dissertation, Virginia Polytechnic Institute and State University, Blacksburg, VA, 1998.

Doman, D.B. and Anderson, M.R., “Projection Methods for Optimal Pilot Model Order Reduction: Optimal versus Suboptimal.” In Proceedings of the 1997 AIAA Atmospheric Flight Mechanics Conference, New Orleans LA, AIAA 97-3500, August 1997,

Doman, D.B. and Anderson, M.R., “Fixed Order Optimal Pilot Models.” In Proceedings of the 1996 AIAA Guidance, Navigation and Control Conference, San Diego, CA, AIAA 96-3871, August 1996.

Doman, D.B., “Interactive Flying Qualities Toolbox for Matlab User’s Guide: Vol. 1, Short Term Pitch Response Criteria and Modified Optimal Control Pilot Model”, WL-TR 95-3070, Wright Patterson AFB, OH, 1995.

Doman, D.B. and Andrisani, D. A., “Use of a Laboratory Tilt Rotor Aircraft to Develop Practical Knowledge of Flying Qualities Issues”. Proceedings of the 1994 AIAA Guidance, Navigation and Control Conference, Scottsdale, AZ. AIAA Paper 94-3696

Doman, D.B., “An Experimental Study of Pilot/Vehicle Dynamics Using A Laboratory Tilt Rotor Flying Machine”. WL-TR-93-3063, Wright Patterson AFB, OH, 1993

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