Works matching DE "MISSILE control systems"
Results: 45
Two-channel pitch/yaw missile autopilot design using arbitrary order sliding modes based pole placement.
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- Aeronautical Journal, 2015, v. 119, n. 1216, p. 765, doi. 10.1017/S0001924000010812
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Pulse-frequency modulated guidance laws for a mortar missile with a pulse jet control mechanism.
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- Aeronautical Journal, 2015, v. 119, n. 1213, p. 389, doi. 10.1017/S0001924000010526
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Modifying the MARK 6 Guidance System.
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- EE: Evaluation Engineering, 2009, v. 48, n. 10, p. 12
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Common Core ATE For Functional Testing.
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- EE: Evaluation Engineering, 2007, v. 46, n. 8, p. 30
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From the Editor.
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- Air Power History, 2008, v. 55, n. 2, p. 3
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- Article
Raytheon Awarded $349 M U.S. Army Contract for TOW Missiles.
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- Microwave Journal, 2012, v. 55, n. 11, p. 47
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The Ins and Outs of Microwave Signal Capture and Playback.
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- Microwave Journal, 2012, p. 48
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Lockheed Martin Receives $194 M Contract for Army Tactical Missile System.
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- Microwave Journal, 2008, v. 51, n. 3, p. 58
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- Article
Raytheon Awarded $127 M US Army Contract for the Joint SLAMRAAM System.
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- Microwave Journal, 2004, v. 47, n. 5, p. 136
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- Article
Rockwell Collins Joins Northrop Grumman-Raytheon Team.
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- Microwave Journal, 2004, v. 47, n. 3, p. 41
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Handling Unpleasant News In the East German Press.
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- Journalism Quarterly, 1985, v. 62, n. 1, p. 136, doi. 10.1177/107769908506200122
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Update.
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- BioScience, 1981, v. 31, n. 5, p. 360, doi. 10.1093/bioscience/31.5.360
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- Article
Füze Savunma Sistemi ve Türkiye.
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- Middle Eastern Analysis / Ortadogu Analiz, 2011, v. 3, n. 34, p. 74
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Integrated Guidance and Control of Interceptor Missile Based on Asymmetric Barrier Lyapunov Function.
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- International Journal of Aerospace Engineering, 2019, p. 1, doi. 10.1155/2019/8531584
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Active target defence differential game: fast defender case.
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- IET Control Theory & Applications (Wiley-Blackwell), 2017, v. 11, n. 17, p. 2985, doi. 10.1049/iet-cta.2017.0302
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The Modern Roman Circus.
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- Bulletin of the Atomic Scientists, 1957, v. 13, n. 9, p. 331, doi. 10.1080/00963402.1957.11457593
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- Article
Robust Missile Autopilots With Finite-Time Convergence.
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- Asian Journal of Control, 2016, v. 18, n. 3, p. 1010, doi. 10.1002/asjc.1183
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Aircraft Missile Avoidance.
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- Operations Research, 1976, v. 24, n. 3, p. 420, doi. 10.1287/opre.24.3.420
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OPTIMAL ALLOCATION OF MISSILES AGAINST AREA AND POINT DEFENSES.
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- Operations Research, 1971, v. 19, n. 3, p. 605, doi. 10.1287/opre.19.3.605
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EXPECTED RETALIATORY CAPABILITIES OF LAUNCH CONTROL NETWORKS.
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- Operations Research, 1963, v. 11, n. 5, p. 795, doi. 10.1287/opre.11.5.795
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- Article
Pre-emptive Strike against Iran: Prelude to An Avoidable Disaster?
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- Middle East Policy, 2012, v. 19, n. 4, p. 127, doi. 10.1111/j.1475-4967.2012.00565.x
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- Article
Continuous higher order sliding mode control with adaptation of air breathing hypersonic missile.
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- International Journal of Adaptive Control & Signal Processing, 2016, v. 30, n. 8-10, p. 1099, doi. 10.1002/acs.2664
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- Article
Bayesian Stockpile Reliability Methodology for Complex Systems.
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- Military Operations Research, 2007, v. 12, n. 2, p. 25, doi. 10.5711/morj.12.2.25
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Model Following Control Approach for Missile Autopilot Design.
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- Nonlinear Studies, 2004, v. 11, n. 2, p. 227
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Missile Autopilot Design via Approximate Nonlinear Dynamic Inversion.
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- Nonlinear Studies, 2004, v. 11, n. 2, p. 215
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Reduced order H∞ loop-shaping control of a missile pitch axis over a wide flight envelope.
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- Nonlinear Studies, 2004, v. 11, n. 2, p. 199
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Computer-Aided Synthesis of Nonlinear Autopilot for Missiles.
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- Nonlinear Studies, 2004, v. 11, n. 2, p. 173
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Bloodhound on my Trail: Building the Ferranti Argus Process Control Computer.
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- International Journal for the History of Engineering & Technology, 2012, v. 82, n. 1, p. 1, doi. 10.1179/175812111X13188557853928
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Nonsingular Fast Terminal Sliding Mode Control for Spinning Missiles Based on Extended State Observer.
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- International Journal of Pattern Recognition & Artificial Intelligence, 2019, v. 33, n. 1, p. N.PAG, doi. 10.1142/S0218001419590018
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An optimal-fuzzy two-phase CLOS guidance law design using ant colony optimisation.
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- Aeronautical Journal, 2007, v. 111, n. 1124, p. 621, doi. 10.1017/S0001924000004802
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Control of plume inteference effects on axisymmetric afterbodies.
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- Aeronautical Journal, 2004, v. 108, n. 1082, p. 185, doi. 10.1017/S0001924000000099
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Missile Mathematical Model and System Design.
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- AARMS: Academic & Applied Research in Military & Public Management Science, 2017, v. 16, n. 1, p. 29
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COMPARATIVE ANALYSIS OF TUNING MISSILE AUTOPILOTS USING INTELLIGENT METHODS.
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- Scientific Research & Education in the Air Force - AFASES, 2016, v. 1, p. 251, doi. 10.19062/2247-3173.2016.18.1.34
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The Control of Asymmetric Rolling Missiles Based on Improved Trajectory Linearization Control Method.
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- Journal of Aerospace Technology & Management, 2016, v. 8, n. 3, p. 319, doi. 10.5028/jatm.v8i3.617
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Design on a lag-lead emendation network for some missile control system.
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- EURASIP Journal on Wireless Communications & Networking, 2017, v. 2017, n. 1, p. 1, doi. 10.1186/s13638-017-0830-6
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Graphical Visualization of Missile-Target Air-to-Air Engagements: An Educational Tool for Designing and Evaluating Missile Guidance and Control Systems.
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- Computer Applications in Engineering Education, 1995, v. 3, n. 1, p. 5, doi. 10.1002/cae.6180030103
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一种靶弹微波辐射源辅助控制系统的设计.
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- Computer Measurement & Control, 2018, v. 26, n. 5, p. 66, doi. 10.16526/j.cnki.11-4762/tp.2018.05.017
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Intelligent Adaptive Law for Missile Guidance Using Fuzzy Neural Networks.
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- International Journal of Fuzzy Systems, 2013, v. 15, n. 2, p. 182
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Hierarchical anti-disturbance adaptive control for non-linear systems with composite disturbances and applications to missile systems.
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- Transactions of the Institute of Measurement & Control, 2011, v. 33, n. 8, p. 942, doi. 10.1177/0142331210361555
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Double-edged shield.
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- Bulletin of the Atomic Scientists, 2005, v. 61, n. 3, p. 36, doi. 10.2968/061003011
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Hi-tech cattle prod?
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- Bulletin of the Atomic Scientists, 2001, v. 57, n. 3, p. 9
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Not Ready for Prime Time.
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- Bulletin of the Atomic Scientists, 2000, v. 56, n. 5, p. 20, doi. 10.1080/00963402.2000.11456989
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Dynamic surface control and active disturbance rejection control-based integrated guidance and control design and simulation for hypersonic reentry missile.
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- International Journal of Modeling, Simulation & Scientific Computing, 2016, v. 7, n. 3, p. -1, doi. 10.1142/S1793962316500252
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- Article
A Comparative Study of PID, PID with Tracking, and FPID Controller for Missile Canard with аn Optimized Genetic Tuning Method Using Simscape Modelling.
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- Technical Gazette / Tehnički Vjesnik, 2018, v. 25, p. 427, doi. 10.17559/TV-20171207130458
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Northrop Grumman Corporation.
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- Contract Management, 2007, p. 48
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- Article