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

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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

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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

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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

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

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OPTIMAL TERMINAL GUIDANCE WITH CONSTRAINTS AT FINAL TIME.YORK RJ; PASTRICK HL.1977; J. SPACECR. ROCK.; U.S.A.; DA. 1977; VOL. 14; NO 6; PP. 381-383; BIBL. 7 REF.Article

BORESIGHT ERRORS INDUCED BY MISSILE RADOMESSIWIAK K; DOWLING TB; LEWIS LR et al.1979; I.E.E.E. TRANS. ANTENNAS PROPAG.; USA; DA. 1979; VOL. 27; NO 6; PP. 832-841; BIBL. 8 REF.Article