Dr. Ping Lu

Dr. Ping Lu

Professor and Chair Editor-in-Chief, Journal of Guidance, Control, and Dynamics
Academic Affairs
College of Engineering
Department of Aerospace Engineering

SDSU

Email

Primary Email: [email protected]

Phone/Fax

Primary Phone: (619) 594-2278

Building/Location

Engineering - 310
5500 Campanile Drive
San Diego, CA 92182

Files

Bio

Prof. Lu’s current research interests are in advanced guidance of aerospace systems, autonomous trajectory planning and optimization, flight control, and flight mechanics. The research aims at developing theory, methodology, and algorithms for highly constrained missions in a full-spectrum of aerospace applications covering space and atmospheric vehicles, powered flight (by rockets and airbreathing propulsion), and entry/ hypersonic gliding flight.

A hallmark of Prof. Lu’s research program has been meeting real-world challenges with innovative applied research. Prof. Lu has participated in a number of major programs in space transportation systems including the X-33 Advanced Technology Demonstrator, Space Launch Initiative/Next Generation Launch Technology, Orion Crew Exploration Vehicle (now Orion Multi-Purpose Crew Vehicle), and Evolvable Mars Campaign.

Education

  • Ph.D., The University of Michigan

Interests

  • Advanced guidance and control
  • Autonomous trajectory planning, numerical optimal control, flight mechanics
  • Numerical optimal control, flight mechanics
  • Flight mechanics

Awards & Honors

  • NASA Johnson Space Center Director’s Innovation Group Achievement Award, on numerical entry guidance algorithm developed by Prof. Lu (2016)
  • Elected to be a Fellow of American Institute of Aeronautics and Astronautics (AIAA) (2016)
  • AIAA Mechanics and Control of Flight Award, “for contributions in advanced guidance algorithms for entry and ascent flight” (2008)

Presentations

  • Lu, “Assessing Propellant-Optimal Guidance for Crewed Lunar Descent”, AIAA Guidance, Navigation, and Control Conference, January 10, 2025
  • Davami, P. Lu, and A. Rosengren, “Model Predictive Tracking Guidance Applied to Planetary Entry and Powered Descent”, AIAA Guidance, Navigation, and Control Conference, January 10, 2025
  • Sagliano, D. Seelbinder, S. Theil, and P. Lu, “Optimization of Six-Degrees-of-Freedom Entry, Descent, and Landing Trajectory”, AIAA Guidance, Navigation, and Control Conference, January 10, 2025
  • Davami, P. Lu, B. Johnson, and A. Rosengren, “Optimizing End-to-End EDL Trajectories for High-Mass Mars Missions”, AAS Paper 24-043, AAS Guidance and Control Conference, February, 2024
  • Sagliano, D. Seelbinder, S. Theil, B. Johnson, and P. Lu, “Six-Degrees-of-Freedom Aero-Propulsive Entry Trajectory Optimization”, AIAA Paper 2024-1171, AIAA Guidance, Navigation, and Control Conference. January 2024
  • Sagliano, P. Lu, D. Seelbinder, and Stephan Theil, “Six-Degrees-of-Freedom Rocket Landing Optimization by Augmented Convex-Concave Decomposition”, AIAA Paper 2023-2005, AIAA Guidance, Navigation, and Control Conference. January 2023
  • Sandoval, R. A. Lugo, P. Lu, and A. D. Cianciolo, “Simulation Comparison of Entry and Powered Descent Guidance Algorithms for a Human-Scale Mars Mission”, AAS Guidance and Control Conference, AAS Paper 22-042, February 2022
  • Sandoval, P. Lu, J. Hwang, J. Rea, and R. Sostaric, “Multiple Optima in Abort Ascent during Lunar Powered Descent”, AIAA Paper 2022-0949, January 2022
  • Devore, R. Adams, A. Reed, A. Lewis, and P. Lu “Closed-Loop Optimal Control for Spacecraft Rendezvous and Proximity Operations Using Second Order Cone Program”, AAS 21-355, 31st AAS/AIAA Space Flight Mechanics Meeting, Feb. 1-3, 2021
  • Sandoval and P. Lu, “Powered Descent Guidance for a Crewed Lunar Landing Mission”, AAS 2020-044, 43rd Annual AAS Guidance and Control Conference, Jan 31–Feb 5, 2020, Breckenridge, CO
  • Johnson, R. Sostaric, and P. Lu, “Mid Lift-to-Drag Rigid Vehicle 6-DoF Performance for Human Mars Entry, Descent, and Landing: A Fractional Polynomial Powered Descent Guidance Approach”, AIAA 2020-1513, AIAA Atmospheric Flight Mechanics Conference, Jan. 6-10, 2020, Orlando, FL
  • Johnson, P. Lu, B. Nikaido, Z. Hays, and S. D'Souza, “Pterodactyl: Development and Performance of Guidance Algorithms for a Mechanically Deployed Entry Vehicle”, AIAA Guidance, Navigation, and Control Conference, Jan. 6-10, 2020, Orlando, FL.
  • Breanna, P. Lu, and Cerimele, C, “Mid-Lift-to-Drag Ratio Rigid Vehicle 6-DoF EDL Performance Using Tunable Apollo Powered Descent Guidance,” AAS Paper 19–619, AAS/AIAA Astrodynamics Specialist Conference, August 2019, Portland, ME
  • Sun, D. Ran, and P. Lu, “Multi-Phase Spacecraft Mission Optimization by Quadratically Constrained Quadratic Programming”, AIAA Paper 2019-1677, AIAA Guidance, Navigation, and Control Conference, January 2019, San Diego, CA
  • Lu, “Fuel-Optimal and Apollo Powered Descent Guidance Compared for High-Mass Mars Mission” AAS Paper 18-054, AAS Guidance & Control Conference, Breckenridge, CO, Feb. 2018
  • Johnson, E. Braden, R. Sostaric, C. Cerimele, and P. Lu, “Entry, Descent, and Landing Performance for a Mid-Lift-to-Drag Ratio Vehicle at Mars”, AAS Paper 18-053, AAS Guidance & Control Conference, Breckenridge, CO, Feb. 2018.
  • Lu, R. Sostaric, and G. Mendeck, “Adaptive Powered Descent Initiation and Fuel-Optimal Guidance for Mars Applications”, AIAA Paper 2018-0616, AIAA Guidance, Navigation, and Control Conference, January 2018.

additional available upon request

Publications

  • Sagliano, P. Lu, D. Seelbinder, and S. Theil, “An Analytical Treatise on Endo-Atmospheric Fuel-Optimal Rocket Landing”,  Journal of Guidance, Control, and Dynamics, accepted for publication, October 2024
  • P. Lu and C. Davami, “Rethinking Propellant-Optimal Powered Descent Guidance”, accepted for publication, Journal of Guidance, Control, and Dynamics, July 2024
  • S. Sandoval, J. Hwang, and P. Lu, “Abort Guidance During Lunar Powered Descent”, Journal of Guidance, Control, and Dynamics, Vol. 47, No. 3, 2024
  • P. Lu, S. Sandoval, and C. Davami, “Fast and Robust Optimization of Full Trajectory From Entry Through Powered Descent”, Journal of Guidance, Control, and Dynamics, Vol. 47, No. 2, 2024
  • M. Sagliano, D. Seelbinder, S. Theil, and P. Lu, “Six-Degree-of-Freedom Rocket Landing Optimization via Augmented Convex-Concave Decomposition”, Journal of Guidance, Control, and Dynamics, Vol. 47, No. 1, pp. 20-35, 2024
  • B. Pan, Y. Ni, Y. Ma, and P. Lu, “Smoothing Homotopy Methods for Solving Nonlinear Optimal Control Problems", Journal of Guidance, Control and Dynamics, Vol. 46, No.8, pp. 1470-1484, 2023
  • P. Lu and R. Callan, “Propellant-Optimal Powered Descent Guidance Revisited”, Journal of Guidance, Control, and Dynamics, Vol. 46, No. 2, pp. 215-230, 2023
  • P. Lu, A. Lewis, R. Adams, M. DeVore, and C. Petersen, “Finite-Thrust Natural Motion Circumnavigation Injection by Convex Optimization”, Journal of Guidance, Control, and Dynamics, Vol. 45, No. 3, 2022, pp. 453-467
  • P. Lu, “Convex-Concave Decomposition of Nonlinear Equality Constraints in Optimal Control,” published online 1 October, 2020, Journal of Guidance, Control, and Dynamics, doi.org/10.2514/1.G005443
  • P. Lu, “Theory of Fractional-Polynomial Powered Descent Guidance”, Journal of Guidance, Control, and Dynamics, doi:10.2514/1.G004556, Vol. 43, No. 3. 2020, pp. 398-409.
  • P. Lu, “Augmented Apollo Powered Descent Guidance”, Journal of Guidance, Control, and Dynamics, Vol. 42, No. 3, 2019, pp. 447-457.
  • C. Wan, D. Dai, and P. Lu, “An Alternating Minimization Algorithm for Polynomial Optimal Control Problems”, Journal of Guidance, Control, and Dynamics, Vol. 42, No. 4, 2019, pp. 723-736
  • B. Pan, X. Pan, and P. Lu, “Finding Best Solution in Low-Thrust Trajectory Optimization by Two-Phase Homotopy”, Journal of Spacecraft and Rockets, Vol. 56, No. 1, 2019, pp.283-291
  • P. Lu, “Propellant-Optimal Powered Descent Guidance”, Journal of Guidance, Control, and Dynamics, Vol. 41, No. 4, 2018, pp. 813-826.
  • R. Pinson and P. Lu, “Trajectory Design Employing Convex Optimization for Landing on Irregularly Shaped Asteroids”, Journal of Guidance, Control, and Dynamics, Vol. 41, No. 6, 2018, pp. 1243-1256.
  • P. Lu, C. Brunner, S. Stachowiak, G. Mendeck, M. Tigges, and C. Cerimele, “Verification of a Fully Numerical Entry Guidance Algorithm”, Journal of Guidance, Control, and Dynamics, Vol. 40, No. 2, pp. 230-247, 2017.
  • X. Liu, P. Lu, and B. Pan, “Survey of Convex Optimization for Aerospace Applications”, Astrodynamics, Vol. 1, No. 1, p. 23-40, 2017
  • X. Liu, Z. Shen, and P. Lu, “Closed-Loop Optimization of Guidance Gain for Constrained Impact”, Journal of Guidance, Control, and Dynamics, Vol. 40, No. 2, pp. 453-460, 2017
  • X. Liu, P. Lu, and B. Pan, "Survey of Convex Optimization for Aerospace Applications", Astrodynamics, Vol. 1., No. 1, 2017, p. 23-40
  • B. Pan, P. Lu, X. Pan, and Y. Ma, “Double-Homotopy Method for Solving Optimal Control Problems”, Journal of Guidance, Control, and Dynamics, Vol. 39, No. 8, 2016
  • P. Lu, Cerimele, C., Tigges, M., and Matz, D., “Optimal Aerocapture Guidance”, Journal of Guidance, Control, and Dynamics, Vol. 38, No. 4, 2015, pp. 553-565
  • P. Lu, “Entry Guidance: A Unified Method”, Journal of Guidance, Control, and Dynamics, Vol. 37, No. 3, 2014, pp. 713—728.
  • X. Liu and P. Lu, “Solving Non-Convex Optimal Control Problems by Convex Optimization”, Journal of Guidance, Control, and Dynamics, Vol. 37, No. 3, 2014, pp. 750-765
  • P. Lu and X. Liu, “Autonomous Trajectory Planning for Rendezvous and Proximity Operations by Conic Optimization”, Journal of Guidance, Control, and Dynamics, Vol. 36, No. 2, 2013, p. 375-389.
  • Brunner, C. and Lu, P. “Comparison of Fully Numerical Predictor-Corrector and Apollo Skip Entry Guidance Algorithms”, The Journal of the Astronautical Sciences, Vol. 59, No. 3, 2012, p. 517-540 (published online 17 July, 2014)
  • P. Lu and B. Pan, “Highly Constrained Optimal Launch Ascent Guidance”, Journal of Guidance, Control, and Dynamics, Vol. 33, No. 2, 2010, pp. 404-414
  • P. Lu, B. Griffin, G. Dukeman, and F. Chavez, “Rapid Optimal Multi-Burn Ascent Planning and Guidance”, Journal of Guidance, Control, and Dynamics, Vol. 31, No. 6, pp. 1656-1664, 2008
  • P. Lu, “Predictor-Corrector Entry Guidance for Low Lifting Vehicles”, Journal of Guidance, Control, and Dynamics, Vol. 31, No. 4, 2008, pp. 1067-1075
  • P. Lu, D. Doman, and J. Schierman, “Adaptive Terminal Guidance for Hypervelocity Impact in Specified Direction”, Journal of Guidance, Control, and Dynamics, Vol. 29, No. 2, 2006, pp. 269-278
  • Z. Shen, and P. Lu, “On-Board Entry Trajectory Planning for Sub-Orbital Flight”, Acta Astronautica, Vol. 56, Issue 6, 2005, pp. 573-591
  • P. Lu, H. Sun, and B. Tsai, “Closed-Loop Endo-Atmospheric Ascent Guidance”, Journal of Guidance, Control, and Dynamics, Vol. 26, No. 2, 2003, pp. 283-294.
  • J. Burken, P. Lu, and Z. Wu, “Two Reconfigurable Flight Control Designs”, Journal of Guidance, Control, and Dynamics, Vol. 24, No. 3, 2001, pp. 482-493.
  • P. Lu, and J. Hanson, “Entry Guidance for the X-33 Vehicle”, Journal of Spacecraft and Rockets, Vol. 35, No. 3, 1998, pp.342-349.
  • P. Lu, “Nonlinear Trajectory Tracking Guidance with Application to a Launch Vehicle,” Journal of Guidance, Control, and Dynamics, Vol. 19, No. 1, 1996, pp. 99-106
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  • P. Lu, “Augmented Apollo Powered Descent Guidance”, in press, Journal of Guidance, Control, and Dynamics, 2018
  • C. Wan, D. Dai, and P. Lu, “An Alternating Minimization Algorithm for Polynomial Optimal Control Problems”, in press, Journal of Guidance, Control, and Dynamics, 2018
  • P. Lu, “Propellant-Optimal Powered Descent Guidance”, Journal of Guidance, Control, and Dynamics, DOI: 10.2514/1.G003243, Vol. 41, No. 4, 2018, pp. 813-826.
  • R. Pinson and P. Lu, “Trajectory Design Employing Convex Optimization for Landing on Irregularly Shaped Asteroids”, Journal of Guidance, Control, and Dynamics, DOI: 10.2514/1.G003045, Vol. 41, No. 6, 2018, pp. 1243-1256.
  • B. Pan, X. Pan, and P. Lu, “Finding Best Solution in Low-Thrust Trajectory Optimization by Two-Phase Homotopy”, Journal of Spacecraft and Rockets, September 2018, DOI 10.2514/1.A34144
  • P. Lu, C. Brunner, S. Stachowiak, G. Mendeck, M. Tigges, and C. Cerimele, “Verification of a Fully Numerical Entry Guidance Algorithm”, Journal of Guidance, Control, and Dynamics, Vol. 40, No. 2, pp. 230-247, 2017.
  • X. Liu, P. Lu, and B. Pan, “Survey of Convex Optimization for Aerospace Applications”, Astrodynamics, Vol. 1, No. 1, p. 23-40, 2017
  • X. Liu, Z. Shen, and P. Lu, “Closed-Loop Optimization of Guidance Gain for Constrained Impact”, Journal of Guidance, Control, and Dynamics, Vol. 40, No. 2, pp. 453-460, 2017.
  • B. Pan, P. Lu, X. Pan, and Y. Ma, “Double-Homotopy Method for Solving Optimal Control Problems”, Journal of Guidance, Control, and Dynamics, Vol. 39, No. 8, 2016
  • X. Liu, Z. Shen, and P. Lu, “Exact Convex Relaxation for Optimal Flight of Aerodynamically Controlled Missiles”, IEEE Transactions on Aerospace and Electronic Systems, Vol. 52, No. 4, 2016, p. 1881-1892,
  • X. Liu, Z. Shen, and P. Lu, “Entry Trajectory Optimization by Second-Order Cone Programming”,
  • Journal of Guidance, Control, and Dynamics, Vol. 39, No. 2, 2016, pp. 227-241
  • P. Lu, “Entry Guidance Using Time-Scale Separation in Gliding Dynamics”, Journal of Spacecraft and Rockets, Vol. 52, No. 4, 2015, pp. 1253-1258
  • P. Lu, Cerimele, C., Tigges, M., and Matz, D., “Optimal Aerocapture Guidance”, Journal of Guidance, Control, and Dynamics, Vol. 38, No. 4, 2015, pp. 553-565
  • X. Liu, Z. Shen, and P. Lu, “Solving the Maximum-Crossrange Problem via Successive Second-Order Cone
  • Programming with Line Search”, Aerospace Science and Technology, Vol. 47, Dec. 2015, pp. 10-20, doi:10.1016/j.ast.2015.09.008
  • P. Lu, “Entry Guidance: A Unified Method”, Journal of Guidance, Control, and Dynamics, Vol. 37, No. 3, 2014, pp. 713—728.
  • X. Liu and P. Lu, “Solving Non-Convex Optimal Control Problems by Convex Optimization”, Journal of Guidance, Control, and Dynamics, Vol. 37, No. 3, 2014, pp. 750-765
  • B. Pan, Z. Chen, P. Lu, and G. Bao, “Reduced Transversality Conditions in Optimal Space Trajectories”, Journal of Guidance, Control, and Dynamics, Vol. 36, No. 5, 2013, p. 1289-1300
  • P. Lu and X. Liu, “Autonomous Trajectory Planning for Rendezvous and Proximity Operations by Conic Optimization”, Journal of Guidance, Control, and Dynamics, Vol. 36, No. 2, 2013, p. 375-389.
  • B. Pan, P. Lu, and Z. Chen, “Three-Dimensional Closed-Form Costate Solutions in Optimal Coast”, Acta Astronautica, Vol. 77, 2012, p. 156-166.
  • C. Brunner and P. Lu, “Comparison of Fully Numerical Predictor-Corrector and Apollo Skip Entry Guidance Algorithms”, The Journal of the Astronautical Sciences, Vol. 59, No. 3, 2012, p. 517-540 (published online 17 July, 2014)
  • M. Baldwin and P. Lu, “Optimal Deorbit Guidance”, Journal of Guidance, Control, and Dynamics, Vol. 35, No. 1, 2012, p. 93-103.
  • B. Pan, P. Lu and Z. Chen, “Coast Arcs in Optimal Multiburn Orbital Transfers”, Journal of Guidance, Control and Dynamics, Vol. 35, No. 2, 2012, p. 451-461.
  • S. Xue and P. Lu, “Constrained Predictor-Corrector Entry Guidance”, Journal of Guidance, Control, and Dynamics, Vol.33, No. 4, 2010, pp. 1273-1280
  • P. Lu and S. Xue, “Rapid Generation of Accurate Entry Landing Footprints”, Journal of Guidance, Control, and Dynamics, Vol. 33, No. 3, 2010, pp. 756-767
  • P. Lu and B. Pan, “Highly Constrained Optimal Launch Ascent Guidance”, Journal of Guidance, Control, and Dynamics, Vol. 33, No. 2, 2010, pp. 404-414
  • B. Rademacher, P. Lu, A. Strahan, and C. Cerimele, “In-flight Trajectory Planning and Guidance for Autonomous Parafoils”, Journal of Guidance, Control, and Dynamics, Vol. 32, No. 6, 2009, pp. 1697-1712
  • L. Zhu, P. Lu, Z. Jing and S. Hu, “A New Robust Adaptive Control Scheme for Non-Affine Nonlinear Systems Based on SHLNN Disturbance Observer”, International Journal of Innovative Computing, Information and Control, 2009
  • P. Lu, B. Griffin, G. Dukeman, and F. Chavez, “Rapid Optimal Multi-Burn Ascent Planning and Guidance”, Journal of Guidance, Control, and Dynamics, Vol. 31, No. 6, pp. 1656-1664, 2008
  • C. Brunner and P. Lu, “Skip Entry Trajectory Planning and Guidance”, Journal of Guidance, Control, and Dynamics, Vol., 31, No. 5, 2008, pp. 1210-1219.
  • P. Lu, “Predictor-Corrector Entry Guidance for Low Lifting Vehicles”, Journal of Guidance, Control, and Dynamics, Vol. 31, No. 4, 2008, pp. 1067-1075
  • L. Zhang and P. Lu, “Fixed-Point Algorithms for Optimal Trajectories of Launch Vehicles”, Engineering
  • Optimization, Vol. 40, No. 4, 2008, pp. 361-381
  • P. Lu, “Asymptotic Analysis of Quasi-Equilibrium Glide in Lifting Entry Flight”, Journal of Guidance, Control, and Dynamics, Vol. 29, No. 3, 2006, pp. 662-670.
  • P. Lu, D. Doman, and J. Schierman, “Adaptive Terminal Guidance for Hypervelocity Impact in Specified Direction”, Journal of Guidance, Control, and Dynamics, Vol. 29, No. 2, 2006, pp. 269-278
  • Z. Shen, and P. Lu, “On-Board Entry Trajectory Planning for Sub-Orbital Flight”, Acta Astronautica, Vol. 56, Issue 6, 2005, pp. 573-591
  • Z. Shen, and P. Lu, “Dynamic Lateral Guidance Logic”, (invited paper in a special section on Reusable Launch Vehicle Guidance and Control), Journal of Guidance, Control, and Dynamics, Vol. 27, No. 6, 2004, pp. 949-959.
  • P. Lu, H. Sun, and B. Tsai, “Closed-Loop Endo-Atmospheric Ascent Guidance”, Journal of Guidance, Control, and Dynamics, Vol. 26, No. 2, 2003, pp. 283-294.
  • Z. Shen, and P. Lu, “On-Board Generation of Three-Dimensional Constrained Entry Trajectories”, Journal of Guidance, Control, and Dynamics, Vol. 26, No. 1, 2003, pp. 111-121.
  • P. Lu, and Z. Shen, “A Unifying Treatment to Control of Nonlinear Systems with Two Time Scales”, Journal of Guidance, Control, and Dynamics, Vol. 25, No. 5, 2002, pp 975-979.
  • J. Burken, P. Lu, Z. Wu, and C. Bahm, “Two Reconfigurable Flight-Control Design Methods: Servomechanism and Control Allocation”, Journal of Guidance, Control, and Dynamics, Vol. 24, No. 3, 2001, pp. 482-493.
  • P. Lu, “Closed-Form Control Laws for Linear Time-Varying Systems”, IEEE Transactions on Automatic Control, Vol. 45, No. 3, 2000, pp. 537-542.
  • L. Tian, P. Lu, and J. Burken, “Nonlinear Engine-Only Flight Control”, Nonlinear Problems in Aviation and Aerospace, edited by S. Sivasundaram, Gordon and Breach Science Publishers, London, U. K., 1999.
  • P. Lu, “Regulation about Time-Varying Trajectories: Precision Entry Guidance Illustrated”, Journal of Guidance, Control, and Dynamics, Vol. 22, No. 6, 1999, pp. 784-790.
  • P. Lu and J. Burken, “Controlling Aircraft with Engine Thrust Only: Nonlinear Challenges”, Nonlinear Analysis, Vol. 35, 1999, pp. 21-35.
  • P. Lu, “Approximate Nonlinear Receding-Horizon Control Laws in Closed Form”, International Journal of Control (IJC), Vol. 71, No. 1, 1998, pp. 19-34.
  • P. Lu, and J. Hanson, “Entry Guidance for the X-33 Vehicle”, Journal of Spacecraft and Rockets, Vol. 35, No. 3, 1998, pp.342-349.
  • P. Lu, “Intercept of Nonmoving Targets at Arbitrary Time-Varying Velocity”, Journal of Guidance, Control, and Dynamics, Vol. 21, No. 1, pp. 176-178, 1998.
  • P. Lu, “Nonlinear Systems with Control and State Constraints”, Optimal Control Applications and Methods, Vol. 18, 1997, pp. 313-326.
  • P. Lu, “Optimal Semi-Analytical Guidance for Reentry Flight”, Space Technology, Vol. 17, No. 1, 1997, pp. 7-14.
  • P. Lu, “Tracking Control of Nonlinear Systems with Bounded Controls and Control Rates”, Automatica, Vol. 22, No. 6, pp. 1199-1202, 1997.
  • P. Lu, “Entry Guidance and Trajectory Control for Reusable Launch Vehicle,” Journal of Guidance, Control, and Dynamics, Vol. 20, No. 1, pp. 143-149, 1997.
  • P. Lu, “Constrained Tracking Control of Nonlinear Systems,” Systems and Control Letters, Vol. 27, 1996, pp. 305-314.
  • P. Lu and B. L. Pierson, “Optimal Aircraft Terrain-Following with Nonlinear Engine Dynamics,” Journal of Guidance, Control, and Dynamics, Vol. 19, No. 1, 1996, pp. 240-242.
  • P. Lu, “Nonlinear Trajectory Tracking Guidance with Application to a Launch Vehicle,” Journal of Guidance, Control, and Dynamics, Vol. 19, No. 1, 1996, pp. 99-106.
  • P. Lu and B. L. Pierson, “Aircraft Terrain-Following Based on a Nonlinear Continuous Predictive Control Approach”, Journal of Guidance, Control, and Dynamics, Vol. 17, No. 4, pp. 817-823, 1995.
  • P. Lu, “Optimal Predictive Control of Nonlinear Continuous Systems”, International Journal of Control, Vol. 62, No. 3, 1995, pp. 633-649.
  • P. Lu and B.L. Pierson, “Optimal Terrain-Following Analysis and Trajectory Generation”, Journal of Guidance, Control, and Dynamics, Vol. 17, No. 3, pp. 555-560, 1995.
  • K.C. Lin and P. Lu, “Inverse Simulation - An Error Analysis”, Simulation Journal, Vol. 65, No. 6, 1995, p. 385-392.
  • N.X. Vinh, E.G. Gilbert, R.M. Howe, D. Sheu, and P. Lu, “Reachable Domain for Interception at Hyperbolic Speeds”, Acta Astronautica, Vol. 35, No. 1, 1995, pp. 1-8.
  • P. Lu, "Nonlinear Predictive Controllers for Continuous Systems," Journal of Guidance, Control and Dynamics, Vol. 17, No. 3, 1994, pp. 553-560.
  • P. Lu, and M. Asif Khan, "Nonsmooth Trajectory Optimization: An Approach Using Continuous Simulated Annealing," Journal of Guidance, Control, and Dynamics, Vol. 17, No. 4, 1994, pp. 685-691.
  • M. Asif Khan, and P. Lu, "New Technique for Nonlinear Control of Aircraft," Journal of Guidance, Control, and Dynamics, Vol. 17, No. 5, 1994.
  • P. Lu, and K. C. Lin, "Nonlinear Control of an Autonomous Tracked Vehicle," Transactions of the Institute of Measurement and Control, Vol. 16, No. 5, 1994.
  • P. Lu, "Analytical Solution to Constrained Hypersonic Trajectories," Journal of Guidance, Control and Dynamics , Vol. 16, No. 5, 1993, pp. 956-960.
  • P. Lu, and N. X. Vinh, "On the Minimax Optimal Control Problem and Its Variations," Optimal Control ---
  • International Series of Numerical Mathematics, Vol. 111, ed. by Klaus H. Well, Birkhauser Verlag, Germany, 1993, pp. 99-112.
  • P. Lu, "Inverse Dynamics Approach to Trajectory Optimization for an Aerospace Plane," Journal of Guidance, Control and Dynamics, Vol. 16, No. 4, 1993, pp. 726-732.
  • P. Lu, "A New Nonlinear Optimal Feedback Control Law," Control-Theory and Advanced Technology, Vol. 9, No. 4, 1993, pp. 947-954.
  • K-C Lin, and P. Lu, "State-Tracking Controller Design for A Tracked Vehicle", Journal of Control Systems and Technology", Vol. 1, No. 4, 1993, pp. 297-302.
  • P. Lu, "Use of Approximate Gradients in Trajectory Optimization," Journal of Guidance, Control and Dynamics, Vol. 15, No. 5, 1992, pp. 1299-1301.
  • P. Lu, "Optimal Feedback Control Laws Using Nonlinear Programming," Journal of Optimization Theory and Applications (JOTA), Vol. 71, No. 3, 1991, pp. 599-611.
  • P. Lu and N. X. Vinh, “Optimal Control Problems with Maximum Functional," Journal of Guidance, Control, and Dynamics, Vol. l4, No. 6, 1991, pp. 1215-1223.
  • E. G. Gilbert, R. M. Howe, P. Lu, and N. X. Vinh, "Optimal Aeroassisted Intercept Trajectories at Hyperbolic Speeds," Journal of Guidance, Control, and Dynamics, Vol. 14, No. 1, 1991, pp. 1215-1223.
  • N. X. Vinh, P. Lu, R. M. Howe and E. G. Gilbert, "Optimal Interception with Time Constraint," Journal of Optimization Theory and Applications, Vol. 66, No. 3, 1990, pp. 361-390.
  • P. Lu and N. X. Vinh, “Minimax Optimal Control for Atmospheric Fly-Through Trajectories,” Journal of Optimization Theory and Applications, Vol. 57, No. 1, 1988, pp. 41-58.
  • N. X. Vinh and P. Lu, "Chebyshev Minimax Problems for Skip Trajectories,” The Journal of the Astronautical Sciences (JAS), Vol. 36, No. 102, 1988, pp. 179-197.
  • N. X. Vinh and P. Lu, "Necessary Conditions for Maximax Problems with Application to Aeroglide of Hypervelocity Vehicles,” Acta Astronautica, Vol. 15, No. 5-6, 1987, pp. 413-420.