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

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

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

SENSITIVITY OF HIGHER ORDER HOMING GUIDANCE LAWS TO PARAMETER VARIATIONSROGERS RM.1982; INSTITUTE OF ELECTRICAL AND ELECTRONIC ENGINEERS. SOUTHEASTCON '82 CONFERENCE/1982-04-04/DESTIN FL; USA; NEW YORK: IEEE; DA. 1982; PP. 287-290; BIBL. 4 REF.Conference Paper

GUIDANCE AND CONTROL ASPECTS OF TACTICAL AIR-LAUNCHED MISSILESGONZALEZ JM.1980; ; FRA; NEUILLY-SUR-SEINE: AGARD; DA. 1980; AGARD-AR/154; 9 P.; 30 CM; ISBN 92-835-1372-XReport

WIND TUNNEL DETERMINATION OF THE DRAG OF AN ADVANCED AIR BREATHING MISSILEHILL SC JR.1978; AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS AEROSPACE SCIENCES MEETING. 16/1978/HUNTSVILLE AL; USA; NEW YORK: AIAA; DA. 1978; 78-118; 5 P.Conference Paper

IDENTIFICATION OF POLYNOMIAL COEFFICIENTS OF A MISSILE SYSTEM USING FLIGHT TRIALS DATA.CROMBIE D.1976; IN: OPTIMIZATION ACTION. CONF. OPTIMIZATION ACTION. PROC.; BRISTOL; 1975; LONDON; ACAD. PRESS; DA. 1976; PP. 574-597; BIBL. 1 REF.Conference Paper

INTEGRAL GUIDANCE FOR BALLISTIC MISSILES.BISHOP CM.1976; IN: CONF. DECIS. CONTROL. SYMP. ADAPT. PROCESSES. 15. PROC.; CLEARWATER, FLA.; 1976; NEW YORK; INST. ELECTR. ELECTRON. ENG.; DA. 1976; PP. 1159-1163Conference Paper

MORPHOLOGICAL THINKING ON THE SYNTHESIS OF A BEAM-RIDING MISSILE SYSTEM.MAHAPATRA PR.1976; J. INSTIT. ELECTRON. TELECOMMUNIC. ENGRS; INDIA; DA. 1976; VOL. 22; NO 10; PP. 689-693; BIBL. 4 REF.Article

ON MISSILE STABILITY.WU JJ.1976; J. SOUND VIBR.; G.B.; DA. 1976; VOL. 49; NO 1; PP. 141-147; BIBL. 9 REF.Article

APPLICATION OF ANGLE-ONLY TRACK TO BALLISTIC MISSILE DEFENSE.WEINER LB; HOMSLEY TL.1976; IN: CONF. DECIS. CONTROL. SYMP. ADAPT. PROCESSES. 15. PROC.; CLEARWATER, FLA.; 1976; NEW YORK; INST. ELECTR. ELECTRON. ENG.; DA. 1976; PP. 579-584; BIBL. 9 REF.Conference Paper

RELATIONS BETWEEN DISTURBANCE-UTILIZING CONTROL AND CERTAIN WELL-KNOWN HOMING MISSILE GUIDANCE LAWSKELLY WC.1982; INSTITUTE OF ELECTRICAL AND ELECTRONIC ENGINEERS. SOUTHEASTCON '82 CONFERENCE/1982-04-04/DESTIN FL; USA; NEW YORK: IEEE; DA. 1982; PP. 15-17; BIBL. 8 REF.Conference Paper

GENERALIZED MICROCOMPUTER-BASED HARPOON MISSILE SIMULATION TRAINERLEONARD JV; CROSBY HA.1980; ANNUAL SIMULATION SYMPOSIUM. 13/1980/TAMPA FL; USA; TAMPA: ANNUAL SIMULATION SYMPOSIUM; DA. 1980; PP. 271-290Conference Paper

ON VALIDATING SIMULATION MODELS OF MISSILE SYSTEMS.KHEIR NA; HOLMES WM.1978; SIMULATION; USA; DA. 1978; VOL. 30; NO 4; PP. 117-128; BIBL. 2 P.Article

PROCESS MODELLING FOR THE DESIGN OF CONTROL SYSTEMSRUBIN O.1978; TRANS. S. AFR. INST. ELECTR. ENGRS; ZAF; DA. 1978; VOL. 69; NO 8; PP. 253-262; ABS. AFR; BIBL. 8 REF.Article

MATERIALS AND PROCESSES FOR THE TOMAHAWK CRUISE MISSILE.TORGERSON RT; CHRISTIAN JL.1978; METAL PROGR.; U.S.A.; DA. 1978; VOL. 113; NO 3; PP. 52-58Article

MISSILE AERODYNAMIC SENSITIVITY ANALYSISQUAM DL.1978; AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS AEROSPACE SCIENCES MEETING. 16/1978/HUNTSVILLE AL; USA; NEW YORK: AIAA; DA. 1978; 78-113; 10 P.; BIBL. 6 REF.Conference Paper

SIMULATION-SYSTEMS ANALYSIS TOOLS FOR A/A MISSILE DESIGN.EICHLER J.1977; CANAD. AERONAUT. SPACE J.; CANADA; DA. 1977; VOL. 23; NO 6; PP. 372-389; BIBL. 8 REF.Article

GENERAL PURPOSE TACTICAL MISSILE: SIMULATION PROGRAMAKISHITA S.1980; ANNUAL SIMULATION SYMPOSIUM. 13/1980/TAMPA FL; USA; TAMPA: ANNUAL SIMULATION SYMPOSIUM; DA. 1980; PP. 257-270Conference Paper

OPTIMIZATION OF MISSILE TRAJECTOIRES BY MEANS OF EVOLUTION STRATEGYGAIDOSCH H.1980; AEROSPACE SCIENCES MEETING. 18/1980/PASADENA CA; USA; NEW YORK: AIAA; DA. 1980; 10 P.; BIBL. 2 REF.Conference Paper

WIND-TUNNEL INVESTIGATION OF DIFFERENT MISSILE CONFIGURATIONS AT ANGLES OF ATTACK UP TO 30 DEGREES AND MACH NUMBERS 0.6 TO 3.5ENDMANN P.1978; AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS AEROSPACE SCIENCES MEETING. 16/1978/HUNTSVILLE AL; USA; NEW YORK: AIAA; DA. 1978; 78-22; 7 P.; BIBL. 2 REF.Conference Paper

ESTIMATION OF OBSTACLE AND TERRAIN IMPACT PROBABILITIES.SWANSON RS; MUSA SA.1976; J. SPACECR. ROCK.; U.S.A.; DA. 1976; VOL. 13; NO 6; PP. 356-361; BIBL. 6 REF.Article

NONLINEAR ROLLING MOTION OF A CANARD-CONTROLLED MISSILE CONFIGURATION AT ANGLES OF ATTACK FROM 0 TO 30 DEGREES IN INCOMPRESSIBLE FLOWHARDY SR.1978; AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS AEROSPACE SCIENCES MEETING. 16/1978/HUNTSVILLE AL; USA; NEW YORK: AIAA; DA. 1978; 78-61; 10 P.; BIBL. 7 P.Conference Paper

MISSILE AERODYNAMICS/FLUID DYNAMICS PANEL, ANKARA, 5-6 MARCH (1978), ROME, 8-9 MARCH (1978), RHODE-SAINT-GENESE, 12-16 MARCH (1978)1979; MISSILE AERODYNAMICS. FLUID DYNAMICS PANEL/1978-03-05/ANKARA; FRA; NEUILLY SUR SEINE: AGARD; DA. 1979; PAG. MULT.: ILL.; 30 CM; BIBL. DISSEM.; ISBN 92-835-0234-5Conference Proceedings