Tactical and strategic missile guidance P Zarchan American Institute of Aeronautics and Astronautics, Inc., 2012 | 2199 | 2012 |
Progress in astronautics and aeronautics: fundamentals of Kalman filtering: a practical approach P Zarchan Aiaa, 2005 | 1231 | 2005 |
Tactical and strategic missile guidance P Zarchan Progress in astronautics and aeronautics 176, 143-154, 1997 | 581 | 1997 |
A new look at classical vs modern homing missile guidance FW Nesline, P Zarchan Journal of Guidance and Control 4 (1), 78-85, 1981 | 267 | 1981 |
Proportional navigation and weaving targets P Zarchan Journal of Guidance, Control, and Dynamics 18 (5), 969-974, 1995 | 172 | 1995 |
Tactical and strategic missile guidance, American Institute of Aeronautics and Astronautics P Zarchan Inc.: Reston, VA, USA 555, 2012 | 164 | 2012 |
Tactical and Strategic Misssile Guidance P Zarchan Progress in astronautics and aeronautics 176, Chap. 3, 1997 | 123* | 1997 |
Tactical and Strategic Missile Guidance, Vol. 157 P Zarchan Progress in Astronautics and Aeronautics, AIAA, Washington, DC, 17-35, 1994 | 113 | 1994 |
Fundamentals of Kalman Filtering—A Practical Approach. American Institute of Aeronautics and Astronautics P Zarchan, H Musoff Inc, 2005 | 95 | 2005 |
Why modern controllers can go unstable in practice FW Nesline, P Zarchan Journal of Guidance, Control, and Dynamics 7 (4), 495-500, 1984 | 94 | 1984 |
Complete statistical analysis of nonlinear missile guidance systems-SLAM P Zarchan Journal of guidance and control 2 (1), 71-78, 1979 | 90 | 1979 |
Radome induced miss distance in aerodynamically controlled homing missiles F Nesline, P Zarchan 17th Fluid Dynamics, Plasma Dynamics, and Lasers Conference, 1845, 1984 | 89 | 1984 |
Alternative approach to the solution of Lambert's problem SL Nelson, P Zarchan Journal of Guidance, Control, and Dynamics 15 (4), 1003-1009, 1992 | 88 | 1992 |
Representation of realistic evasive maneuvers by the use of shaping filters P Zarchan Journal of Guidance and Control 2 (4), 290-295, 1979 | 86 | 1979 |
Combined optimal/classical approach to robust missile autopilot design FW Nesline, BH Wells, P Zarchan Journal of Guidance and Control 4 (3), 316-322, 1981 | 83 | 1981 |
Line-of-sight reconstruction for faster homing guidance FW Nesline, P Zarchan Journal of Guidance, Control, and Dynamics 8 (1), 3-8, 1985 | 69 | 1985 |
Adaptive radome compensation using dither P Zarchan, H Gratt Journal of Guidance, Control, and Dynamics 22 (1), 51-57, 1999 | 58 | 1999 |
Missile guidance design tradeoffs for high-altitude air defense FW Nesline, P Zarchan Journal of Guidance, Control, and Dynamics 6 (3), 207-212, 1983 | 58 | 1983 |
Miss distance dynamics in homing missiles FW Nesline, P Zarchan 17th Fluid Dynamics, Plasma Dynamics, and Lasers Conference, 1844, 1984 | 55 | 1984 |
Ballistic missile defense guidance and control issues P Zarchan Science & Global Security 8 (1), 99-124, 1999 | 52 | 1999 |