Pascal and Francis Bibliographic Databases

Help

Search results

Your search

kw.\*:("Missiles")

Filter

A-Z Z-A Frequency ↓ Frequency ↑
Export in CSV

Document Type [dt]

A-Z Z-A Frequency ↓ Frequency ↑
Export in CSV

Publication Year[py]

A-Z Z-A Frequency ↓ Frequency ↑
Export in CSV

Discipline (document) [di]

A-Z Z-A Frequency ↓ Frequency ↑
Export in CSV

Language

A-Z Z-A Frequency ↓ Frequency ↑
Export in CSV

Author Country

A-Z Z-A Frequency ↓ Frequency ↑
Export in CSV

Origin

A-Z Z-A Frequency ↓ Frequency ↑
Export in CSV

Results 1 to 25 of 1444

  • Page / 58
Export

Selection :

  • and

Adaptive critic-based neural networks for agile missile controlDONGCHEN HAN; BALAKRISHNAN, S. N.Journal of guidance, control, and dynamics. 2002, Vol 25, Num 2, pp 404-407, issn 0731-5090Conference Paper

Impact time control guidance law with field of view constraintYOUAN ZHANG; XINGLIANG WANG; HUALI WU et al.Aerospace science and technology (Imprimé). 2014, Vol 39, pp 361-369, issn 1270-9638, 9 p.Article

Development of three-dimensional aiming point guidance lawLIN, Yu-Ping; TSAO, Lu-Ping; LIN, Chun-Liang et al.International journal of systems science. 2010, Vol 41, Num 11, pp 1353-1362, issn 0020-7721, 10 p.Article

Stability of modern guidance laws with model mismatchWEISS, Haim; HEXNER, Gyorgy.American Control Conference. 2004, pp 3634-3639, isbn 0-7803-8335-4, 6 p.Conference Paper

AN EFFECTIVE ENVIRONMENTAL CONTROL SYSTEM FOR A SUPERSONIC AIR-LAUNCHED MISSILEGONZALEZ JI.1981; ISA TRANS.; ISSN 0019-0578; USA; DA. 1981; VOL. 20; NO 4; PP. 95-103; BIBL. 1 REF.Article

POWERED-FLIGHT TRAJECTORY OPTIMIZATION FOR AN INERTIAL-GUIDANCE BALLISTIC VEHICLE = OPTIMISATION DE LA TRAJECTOIRE DE VOL PROPULSE D'UN VEHICULE BALISTIQUE A GUIDAGE INERTIELHOY EC; LEONDES CT.1972; ASTRONAUT. ACTA; G.B.; DA. 1972; VOL. 17; NO 6; PP. 857-870; ABS. FR. ALLEM.; BIBL. 3 REF.Serial Issue

New criterion for aircraft susceptibility to infrared guided missilesARVIND RAO, G; MAHULIKAR, Shripad P.Aerospace science and technology. 2005, Vol 9, Num 8, pp 701-712, issn 1270-9638, 12 p.Article

Terminal guidance laws of missile based on ISMC and NDOB with impact angle constraintZHENXING ZHANG; SHIHUA LI; SHENG LUO et al.Aerospace science and technology (Imprimé). 2013, Vol 31, Num 1, pp 30-41, issn 1270-9638, 12 p.Article

Kill Vehicle Guidance and Control Sizing for Boost-Phase InterceptZARCHAN, Paul.Journal of guidance, control, and dynamics. 2011, Vol 34, Num 2, pp 513-521, issn 0731-5090, 9 p.Article

Dither-based compensating strategy for radome boresight error and gimbal frictionLIN, Y.-C; LIN, C.-L; SHI, W.-C et al.Aeronautical Journal. 2008, Vol 112, Num 1138, pp 715-723, issn 0001-9240, 9 p.Article

Depth Control of the Brennan TorpedoDENNY, Mark.IEEE control systems. 2011, Vol 31, Num 1, pp 66-73, issn 1066-033X, 8 p.Article

Approaches to roll-loop design for BTT CLOS guidanceRODDY, D. J; IRWIN, G. W; WILSON, H et al.IEE proceedings. Part D. Control theory and applications. 1985, Vol 132, Num 6, pp 268-276, issn 0143-7054Article

Fluidic thrust vector controlHALOULAKOS, V. E.Fluidics quarterly. 1983, Vol 15, Num 3, pp 39-65, issn 0015-4687Article

ZUM KOLLISIONSKWS BEDINGUNGEN, LENKGESETZE UND EIGENSCHAFTEN = LA COURSE VERS LA COLLISION. CONDITIONS, LOIS DE GUIDAGE ET PROPRIETESHOFMANN W.1980; D.F.V.L.R. FORSCH.-BER.; DEU; DA. 1980; NO 6; 107 P.; ABS. ENG; BIBL. 8 REF.Serial Issue

THE RISING IMPORTANCE OF RADAR IN TACTICAL MISSILESCURRIE MR.1980; MICROWAVE J.; USA; DA. 1980; VOL. 23; NO 8; PP. 16-70; 1P.Article

Ring wing for a compressed missileAUGUST, H; HARDY, F. W; OSBORN, R et al.Journal of aircraft. 1996, Vol 33, Num 4, pp 837-839, issn 0021-8669Article

Can Lead-Lag Guidance Compensator Guarantee Zero Miss Distance?GUTMAN, Shaul.Journal of guidance, control, and dynamics. 2008, Vol 31, Num 3, pp 779-782, issn 0731-5090, 4 p.Article

Multistepping approach to finite-interval missile integrated controlVADDI, S. S; MENON, P. K; SWERIDUK, G. D et al.Journal of guidance, control, and dynamics. 2006, Vol 29, Num 4, pp 1015-1018, issn 0731-5090, 4 p.Article

Differential geometric guidance based on the involute of the target's trajectory : 2-D aspectsARIFF, O; ZBIKOWSKI, R; TSOURDOS, A et al.American Control Conference. 2004, pp 3640-3645, isbn 0-7803-8335-4, 6 p.Conference Paper

Structured multivariable phase margin analysis with applications to a missile autopilotBAR-ON, Jonathan R; ADAMS, Robert J.Journal of guidance, control, and dynamics. 2003, Vol 26, Num 2, pp 363-366, issn 0731-5090, 4 p.Article

The design of an IR/video imaging feature-based Autotracker for the macintosh-hosted G4 processorMILLS, Samuel T; HALL, Robert L.SPIE proceedings series. 2001, pp 58-62, isbn 0-8194-4060-4Conference Paper

Testing a course control algorithm in the presence of jammingNEZHINSKII, N. N; VIKULOV, O. V.Radio and communications technology. 1999, Vol 4, Num 2, pp 93-99, issn 1087-7126Article

A rapid and high precise calibration method for long-distance cruise missilesWANG XINLONG; WANG BIN; WU XIAOJUAN et al.Aerospace science and technology (Imprimé). 2013, Vol 27, Num 1, pp 1-9, issn 1270-9638, 9 p.Article

Optimal guidance law for cooperative attack of multiple missiles based on optimal control theoryXIAO SUN; YUANQING XIA.International journal of control. 2012, Vol 85, Num 7-9, pp 1063-1070, issn 0020-7179, 8 p.Article

Compensation of actuator dynamics in nonlinear missile controlCHWA, Dongkyoung; JIN YOUNG CHOI; SEO, Jin H et al.IEEE transactions on control systems technology. 2004, Vol 12, Num 4, pp 620-626, issn 1063-6536, 7 p.Article

  • Page / 58