Works matching Missile control systems

Results: 136

Design on a lag-lead emendation network for some missile control system.

Published in:

EURASIP Journal on Wireless Communications & Networking, 2017, v. 2017, n. 1, p. 1, doi. 10.1186/s13638-017-0830-6

By:

Guo, Xiwei;
Li, Zhuo;
Zhai, You;
Liu, Deliang

Publication type:

Article

Graphical Visualization of Missile-Target Air-to-Air Engagements: An Educational Tool for Designing and Evaluating Missile Guidance and Control Systems.

Published in:

Computer Applications in Engineering Education, 1995, v. 3, n. 1, p. 5, doi. 10.1002/cae.6180030103

By:

Rodriguez, Armando A.;
Aguilar, Ricardo

Publication type:

Article

基于状态输出反馈自适应模糊控制的导弹控制系统设计.

Published in:

Aero Weaponry, 2023, v. 30, n. 6, p. 50, doi. 10.12132/ISSN.1673-5048.2022.0239

By:

黄睿涵;
段朝阳;
李海峰

Publication type:

Article

DESIGN AND THERMAL ANALYSIS OF IMPULSE THRUSTERS FOR CONTROL SYSTEMS OF GUIDED MISSILES.

Published in:

Thermal Science, 2025, v. 29, n. 1B, p. 651, doi. 10.2298/TSCI240912284A

By:

ALLOUCHE, Toufik;
ŽIVKOVIĆ, Saša Ž.;
FERFOURI, Abdellah;
JERKOVIĆ, Damir D.;
HRISTOV, Nebojša P.;
KARIĆ, Marko Z.

Publication type:

Article

Pulse-frequency modulated guidance laws for a mortar missile with a pulse jet control mechanism.

Published in:

Aeronautical Journal, 2015, v. 119, n. 1213, p. 389, doi. 10.1017/S0001924000010526

By:

Pavic, M.;
Pavkovic, B.;
Mandic, S.;
Zivkovic, S.;
Cuk, D.

Publication type:

Article

模型大不确定下的导弹姿态控制系统设计.

Published in:

Journal of Ordnance Equipment Engineering, 2023, v. 44, n. 3, p. 191, doi. 10.11809/bqzbgcxb2023.03.027

By:

周航;
张文杰;
周建平;
夏群利

Publication type:

Article

Hierarchical anti-disturbance adaptive control for non-linear systems with composite disturbances and applications to missile systems.

Published in:

Transactions of the Institute of Measurement & Control, 2011, v. 33, n. 8, p. 942, doi. 10.1177/0142331210361555

By:

Guo, Lei;
Wen, Xin-Yu

Publication type:

Article

Common Core ATE For Functional Testing.

Published in:

EE: Evaluation Engineering, 2007, v. 46, n. 8, p. 30

By:

Kahn, Andrew

Publication type:

Article

基于数传电台的靶弹微波源辅助控制系统设计.

Published in:

Computer Measurement & Control, 2022, v. 30, n. 8, p. 122, doi. 10.16526/j.cnki.11-4762/tp.2022.08.020

By:

王刚;
刘基睿;
杜江

Publication type:

Article

基于自适应干扰观测器的巡航导弹掠海飞行轨迹跟踪控制.

Published in:

Journal of Shanghai University / Shanghai Daxue Xuebao, 2024, v. 30, n. 2, p. 244, doi. 10.12066/j.issn.1007-2861.2326

By:

刘宇;
李妍;
毛科峰;
张丹

Publication type:

Article

超声速巡航导弹速度控制系统设计.

Published in:

Journal of Ballistics / Dandao Xuebao, 2020, v. 32, n. 3, p. 79, doi. 10.12115/j.issn.1004-499X(2020)03-015

By:

邱志强;
廖选平;
孙瑞胜;
朱斌

Publication type:

Article

基于随机鲁棒优化的导弹姿态控制系统设计.

Published in:

Journal of Ballistics / Dandao Xuebao, 2019, v. 31, n. 2, p. 60, doi. 10.12115/j.issn.1004-499X(2019)02-011

By:

徐帅;
高敏;
方丹;
王毅;
赵文栋

Publication type:

Article

Integrated Guidance and Control of Interceptor Missile Based on Asymmetric Barrier Lyapunov Function.

Published in:

International Journal of Aerospace Engineering, 2019, p. 1, doi. 10.1155/2019/8531584

By:

Liu, Xiang;
Liang, Xiaogeng

Publication type:

Article

Adaptive periodic event-triggered control for missile-target interception system with finite-horizon convergence.

Published in:

Transactions of the Institute of Measurement & Control, 2020, v. 42, n. 10, p. 1808, doi. 10.1177/0142331219897186

By:

Duan, Dandan;
Liu, Chunsheng;
Sun, Jingliang

Publication type:

Article

GPU-Accelerated PD-IPM for Real-Time Model Predictive Control in Integrated Missile Guidance and Control Systems.

Published in:

Sensors (14248220), 2022, v. 22, n. 12, p. N.PAG, doi. 10.3390/s22124512

By:

Lee, Sanghyeon;
Lee, Heoncheol;
Kim, Yunyoung;
Kim, Jaehyun;
Choi, Wonseok

Publication type:

Article

COMPARATIVE ANALYSIS OF TUNING MISSILE AUTOPILOTS USING INTELLIGENT METHODS.

Published in:

Scientific Research & Education in the Air Force - AFASES, 2016, v. 1, p. 251, doi. 10.19062/2247-3173.2016.18.1.34

By:

GEORGIEV, Rumen;
KOLEV, Kolyo

Publication type:

Article

微型导弹纵向扰动抑制控制系统设计.

Published in:

Journal of National University of Defense Technology / Guofang Keji Daxue Xuebao, 2021, v. 43, n. 1, p. 7, doi. 10.1187/j.cn.202101002

By:

李彤;
孟志鹏;
吕良;
张士峰

Publication type:

Article

Dynamic surface control and active disturbance rejection control-based integrated guidance and control design and simulation for hypersonic reentry missile.

Published in:

International Journal of Modeling, Simulation & Scientific Computing, 2016, v. 7, n. 3, p. -1, doi. 10.1142/S1793962316500252

By:

Zhang, Cong;
Wu, Yun-Jie

Publication type:

Article

Northrop Grumman Corporation.

Published in:: Contract Management, 2007, p. 48
Publication type:: Article

Distributed optimal event‐triggered cooperative control for nonlinear multi‐missile guidance systems with partially unknown dynamics.

Published in:

International Journal of Robust & Nonlinear Control, 2022, v. 32, n. 15, p. 8369, doi. 10.1002/rnc.6285

By:

Gao, Yuxin;
Liu, Chunsheng;
Duan, Dandan;
Zhang, Shaojie

Publication type:

Article

Cooperative control of multi‐missile systems.

Published in:

IET Control Theory & Applications (Wiley-Blackwell), 2015, v. 9, n. 4, p. 441, doi. 10.1049/iet-cta.2014.0361

By:

Wang, Yongji;
Dong, Shuai;
Ou, Liuli;
Liu, Lei

Publication type:

Article

Velocity Control for Coning Motion Missile System Using Direct Discretization Method.

Published in:

Discrete Dynamics in Nature & Society, 2015, p. 1, doi. 10.1155/2015/716547

By:

Sun, Rui-sheng;
Ming, Chao

Publication type:

Article

From the Editor.

Published in:: Air Power History, 2008, v. 55, n. 2, p. 3
Publication type:: Article

OPTIMAL ALLOCATION OF MISSILES AGAINST AREA AND POINT DEFENSES.

Published in:

Operations Research, 1971, v. 19, n. 3, p. 605, doi. 10.1287/opre.19.3.605

By:

Miercort, Frederic A.;
Soland, Richard M.

Publication type:

Article

Design of Guidance and Control Systems for Tactical Missiles.

Published in:

2020

By:

Anderson, David

Publication type:

Book Review

Two-channel pitch/yaw missile autopilot design using arbitrary order sliding modes based pole placement.

Published in:

Aeronautical Journal, 2015, v. 119, n. 1216, p. 765, doi. 10.1017/S0001924000010812

By:

Kada, B.

Publication type:

Article

An optimal-fuzzy two-phase CLOS guidance law design using ant colony optimisation.

Published in:

Aeronautical Journal, 2007, v. 111, n. 1124, p. 621, doi. 10.1017/S0001924000004802

By:

Nobahari, H.;
Pourtakdoust, S.H.

Publication type:

Article

Control of plume inteference effects on axisymmetric afterbodies.

Published in:

Aeronautical Journal, 2004, v. 108, n. 1082, p. 185, doi. 10.1017/S0001924000000099

By:

Lee, Y.-K.;
Raghunathan, S.;
Benard, E.;
Kim, H.-D.;
Setoguchi, T.

Publication type:

Article

Füze Savunma Sistemi ve Türkiye.

Published in:

Middle Eastern Analysis / Ortadogu Analiz, 2011, v. 3, n. 34, p. 74

By:

Başbaşoğlu, Arif

Publication type:

Article

Modifying the MARK 6 Guidance System.

Published in:

EE: Evaluation Engineering, 2009, v. 48, n. 10, p. 12

By:

Jackson, Todd

Publication type:

Article

战术导弹控制系统犅犐犜设计方法.

Published in:

Computer Measurement & Control, 2022, v. 30, n. 1, p. 135, doi. 10.16526/j.cnki.11-4762/tp.2022.01.021

By:

刘仁浩;
李然;
段宇婷;
姜云涛;
夏金秀

Publication type:

Article

一种靶弹微波辐射源辅助控制系统的设计.

Published in:

Computer Measurement & Control, 2018, v. 26, n. 5, p. 66, doi. 10.16526/j.cnki.11-4762/tp.2018.05.017

By:

陈涛;
杜江

Publication type:

Article

The Control of Asymmetric Rolling Missiles Based on Improved Trajectory Linearization Control Method.

Published in:

Journal of Aerospace Technology & Management, 2016, v. 8, n. 3, p. 319, doi. 10.5028/jatm.v8i3.617

By:

Huadong Sun;
Jianqiao Yu;
Siyu Zhang

Publication type:

Article

The numerical investigation on the rolling decoupling of a canard-controlled missile using the jet control system.

Published in:

Engineering Applications of Computational Fluid Mechanics, 2020, v. 14, n. 1, p. 1062, doi. 10.1080/19942060.2020.1799866

By:

Zhang, Jiawei;
Lei, Juanmian;
Yin, Jintao;
Niu, Jianping

Publication type:

Article

Update.

Published in:: BioScience, 1981, v. 31, n. 5, p. 360, doi. 10.1093/bioscience/31.5.360
Publication type:: Article

防空反导战术级指挥控制目标分配发展研究.

Published in:

Aero Weaponry, 2023, v. 30, n. 4, p. 67, doi. 10.12132/ISSN.1673-5048.2022.0273

By:

刘祥雨;
王刚;
李腾达;
夏智权

Publication type:

Article

A nonlinear disturbance observer-based adaptive integral sliding mode control for missile guidance system.

Published in:

International Journal of General Systems, 2022, v. 51, n. 5, p. 474, doi. 10.1080/03081079.2022.2036139

By:

Gürsoy-Demir, Handan;
Önder Efe, Mehmet

Publication type:

Article

Intelligent Adaptive Law for Missile Guidance Using Fuzzy Neural Networks.

Published in:

International Journal of Fuzzy Systems, 2013, v. 15, n. 2, p. 182

By:

Chi-Hsu Wang;
Kun-Neng Hung

Publication type:

Article

Bayesian Stockpile Reliability Methodology for Complex Systems.

Published in:

Military Operations Research, 2007, v. 12, n. 2, p. 25, doi. 10.5711/morj.12.2.25

By:

Anderson Cook, Christine M.;
Graves, Todd;
Hamada, Michael;
Hengartner, Nicholas;
Johnson, Valen E.;
Reese, C. Shane;
Wilson, Alyson G.

Publication type:

Article

Pragmatic Micawberism? Norm Construction on Ballistic Missiles.

Published in:

Contemporary Security Policy, 2006, v. 27, n. 3, p. 526, doi. 10.1080/13523260601060545

By:

Smith, Mark

Publication type:

Article

Adaptive back-stepping sliding mode attitude control of missile systems.

Published in:

International Journal of Robust & Nonlinear Control, 2013, v. 23, n. 15, p. 1699, doi. 10.1002/rnc.2952

By:

Xia, Yuanqing;
Lu, Kunfeng;
Zhu, Zheng;
Fu, Mengyin

Publication type:

Article

Missile guidance and control systems, George M. Siouris, Springer, New York, NY, 2004, 666pp., Price $299.00, ISBN: 0-387-00726-1.

Published in:

International Journal of Robust & Nonlinear Control, 2006, v. 16, n. 5, p. 283, doi. 10.1002/rnc.1056

By:

Ghose, Debasish

Publication type:

Article

Model Following Control Approach for Missile Autopilot Design.

Published in:

Nonlinear Studies, 2004, v. 11, n. 2, p. 227

By:

Aouf, Nabil;
Paiva, Henrique Mohallem;
Rabbath, C. A.;
Lauzon, Marc

Publication type:

Article

Missile Autopilot Design via Approximate Nonlinear Dynamic Inversion.

Published in:

Nonlinear Studies, 2004, v. 11, n. 2, p. 215

By:

Tsourdos, Antonios;
White, Brian A.

Publication type:

Article

Reduced order H∞ loop-shaping control of a missile pitch axis over a wide flight envelope.

Published in:

Nonlinear Studies, 2004, v. 11, n. 2, p. 199

By:

Farret, D.;
Duc, G.;
Harcaut, J. P.

Publication type:

Article

Computer-Aided Synthesis of Nonlinear Autopilot for Missiles.

Published in:

Nonlinear Studies, 2004, v. 11, n. 2, p. 173

By:

Menon, P. K;
Ohlmeyer, E. J.

Publication type:

Article

Missile Mathematical Model and System Design.

Published in:

AARMS: Academic & Applied Research in Military & Public Management Science, 2017, v. 16, n. 1, p. 29

By:

PAPP, István

Publication type:

Article

Aircraft Missile Avoidance.

Published in:

Operations Research, 1976, v. 24, n. 3, p. 420, doi. 10.1287/opre.24.3.420

By:

Vincent, Thomas L.;
Sticht, Douglas J.;
Peng, Willy Y.

Publication type:

Article

EXPECTED RETALIATORY CAPABILITIES OF LAUNCH CONTROL NETWORKS.

Published in:

Operations Research, 1963, v. 11, n. 5, p. 795, doi. 10.1287/opre.11.5.795

By:

Argabright, L.;
Ahlin, A.C.

Publication type:

Article

Bloodhound on my Trail: Building the Ferranti Argus Process Control Computer.

Published in:

International Journal for the History of Engineering & Technology, 2012, v. 82, n. 1, p. 1, doi. 10.1179/175812111X13188557853928

By:

Aylen, Jonathan

Publication type:

Article