EMPIRICAL SOLAR PROTON MODEL FOR ORBITING SPACECRAFT APPLICATIONS.STASSINOPOULOS EG; KING JH.1974; I.E.E.E. TRANS. AEROSPACE ELECTRON. SYST.; U.S.A.; DA. 1974; VOL. 10; NO 4; PP. 442-450; BIBL. 11 REF.Article

ETUDE SUR UN MODELE DE L'ECOULEMENT AUTOUR DU VAISSEAU COSMIQUE "SOYOUZ" DES GAZ DES MOTEURS DE DIRECTION DU VAISSEAU "APPOLO"ANTOKHIN VM; BALASHOV YU P; GERASIMOV YU I et al.1977; IZVEST. AKAD. NAUK S.S.S.R., MEKH. ZHIDKOSTI GAZA; S.S.S.R.; DA. 1977; NO 3; PP. 124-133; BIBL. 13 REF.Article

IMPROVED SECANT METHOD APPLIED TO BOOST TRAJECTORY OPTIMIZATION.GOTTLIEB RG; FOWLER WT.1977; J. SPACECR. ROCK.; U.S.A.; DA. 1977; VOL. 14; NO 2; PP. 96-101; BIBL. 17 REF.Article

ONE-WAY DOPPLER EXTRACTOR.NOSSEN EJ; STARNER ER.1977; R.C.A. REV.; U.S.A.; DA. 1977; VOL. 38; NO 4; PP. 559-587; BIBL. 4 REF.Article

LOW-COST SPACE TELESCOPE POINTING CONTROL SYSTEM.GLAESE JR; KENNEL HF; NURRE GS et al.1976; J. SPACECR. ROCK.; U.S.A.; DA. 1976; VOL. 13; NO 7; PP. 400-405; BIBL. 9 REF.Article

30- TO 100-KEV PROTONS UPSTREAM FROM THE EARTH'S BOW SHOCK.LIN RP; MENG CI; ANDERSON KA et al.1974; J. GEOPHYS. RES.; U.S.A.; DA. 1974; VOL. 79; NO 4; PP. 489-498; BIBL. 10 REF.Article

SUR LA STABILISATION DE LA VIBRATION ELASTIQUE (III).WANG KANG NING; KWAN CHAO CHIH.1976; SCI. SINICA; CHINE; DA. 1976; VOL. 19; NO 3; PP. 323-346; BIBL. 3 REF.Article

AEROELASTIC STABILITY OF THE 747/ORBITER.REDING JP; ERICSSON LE.1977; J. AIRCR.; U.S.A.; DA. 1977; VOL. 14; NO 10; PP. 988-993; BIBL. 14 REF.Article

CONTROL OF UNMANNED SPACE VEHICLES.1975; IN: INT. FED. AUTOM. CONTROL. WORLD CONGR. 6. PROC.; BOSTON-CAMBRIDGE, MASS.; 1975; PITTSBURGH, PA.; INSTRUM. SOC. AM.; DA. 1975; VOL. 4; PP. 14.1.1-14.6.8; BIBL. DISSEM.Conference Paper

OPTIMAL N-IMPULSE TRANSFER TRAJECTORIES USING KUSTAANHEIMO/STIEFEL VARIABLES.JEZEWSKI DJ.1977; A.I.A.A.J., NEW YORK; U.S.A.; DA. 1977; VOL. 15; NO 3; PP. 390-394; BIBL. 5 REF.Article

SHUTTLE ORBITER GUIDANCE SYSTEM FOR THE TERMINAL FLIGHT PHASE.EHLERS HL; KRAEMER JW.1977; AUTOMATICA; G.B.; DA. 1977; VOL. 13; NO 1; PP. 11-21Article

SINGLE-AXIS GYROSCOPIC MOTION WITH UNCERTAIN ANGULAR VELOCITY ABOUT SPIN AXIS.SINGH SN.1977; J. DYNAM. SYST. MEASUR. CONTROL; U.S.A.; DA. 1977; VOL. 99; NO 4; PP. 259-267; BIBL. 11 REF.Article

MINIMUM-TIME RESCUE TRAJECTOIRES BETWEEN SPACECRAFT IN CIRCULAR ORBITS.HOLADAY BH; SWAIM RL.1976; J. SPACECR. ROCK.; U.S.A.; DA. 1976; VOL. 13; NO 7; PP. 393-399; BIBL. 12 REF.Article

SIMULATION IN SUPPORT OF FLIGHT TEST.HANSEN RR; NAGY CJ; KIRSTEN PW et al.1976; A.G.A.R.D. CONF. PROC.; FR.; DA. 1976; NO 198; PP. 10.1-10.28; (FLIGHT SIMULATION-GUIDANCE SYST. SIMULATION. JT. FLIGHT MECH. PANEL-GUIDANCE CONTROL PANEL SYMP.; THE HAGUE; 1975)Conference Paper

SHUTTLE VEHICLE SAFETY ASSURANCE IN UNPOWERED LANDING THROUGH ADAPTIVE CONTROL.ZHEVNIN AA; TOLOKNOV VI; SHEVIAKOV OV et al.1977; J. ASTRONAUT. SCI.; U.S.A.; DA. 1977; VOL. 25; NO 2; PP. 143-149; BIBL. 5 REF.Article

AN OLD DISCIPLINE AND A NEW PHENOMENON: STATIC ELECTRIFICATION AND SPACECRAFT CHARGING.GRARD R; KNOTT K; PEDERSEN A et al.1977; E.S.A. BULL.; FR.; DA. 1977; NO 9; PP. 17-21Article

ATMOSPHERE EXPLORER (AE-C) ADAPTIVE MISSION DESIGN AND TRAJECTORY PERFORMANCE.BARBIERI RW; COOLEY JL; NICKERSON KG et al.1976; ADV. ASTRONAUT. SCI.; U.S.A.; DA. 1976; VOL. 33; PP. 249-261; BIBL. 6 REF.Article

EFFECT OF SPECTRUM ON THE MEASUREMENT OF NOISE.ACKERLIND E.1975; I.E.E.E. TRANS. INSTRUMENT. MEASUR.; U.S.A.; DA. 1975; VOL. 24; NO 2; PP. 118-121; BIBL. 1 REF.Article

THE VALUE OF MULTI-SPACECRAFT MEASUREMENTS.SHEA MA; SMART DF.1974; ASTROPHYS. SPACE SCI. LIBRARY; NETHERL.; DA. 1974; VOL. 42; PP. 381-396; BIBL. 20 REF.; (CORREL. INTERPLANET. MAGNETOSPHERIC OBS. PROC. 7TH ESLAB SYMP.; SAULGAU, WEST GER.; 1973)Conference Paper

DEVELOPMENT OF THE VIKING MARS LANDER THERMAL CONTROL SUBSYSTEM DESIGN.MOREY TF; GORMAN DN.1976; J. SPACECR. ROCK.; U.S.A.; DA. 1976; VOL. 13; NO 4; PP. 229-236; BIBL. 6 REF.Article

SHUTTLE ASCENT TRAJECTORY OPTIMIZATION WITH FUNCTION SPACE QUASI-NEWTON TECHNIQUES.EDGE ER; POWERS WF.1976; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1976; VOL. 14; NO 10; PP. 1369-1376; BIBL. 17 REF.Article

REACTORLESS NUCLEAR PROPULSION*THE LASER ROCKETMINOVITCH MA.sdIN: AM. INST. AERONAUT. ASTRONAUT. SOC. AUTOMOT. ENG. 8TH JOINT PROPUL. SPEC. CONF.; NEW ORLEANS, LA.; 1972; NEW YORK; A.I.A.A.; DA. S.D.; NO 1095; PP. 1-17; BIBL. 1 P. 1/2Conference Paper

STEERING LAW FOR ROOF TYPE CONFIGURATION CONTROL MOMENT GYRO SYSTEM.YOSHIKAWA T.1977; AUTOMATICA; G.B.; DA. 1977; VOL. 13; NO 4; PP. 359-368; BIBL. 11 REF.Article

DETERMINATION OF POLES AND ZEROS OF TRANSFER FUNCTIONS FOR FLEXIBLE SPACECRAFT ATTITUDE CONTROL.OHKAMI Y; LIKINS PW.1976; INTERNATION. J. CONTROL; G.B.; DA. 1976; VOL. 24; NO 1; PP. 13-22; BIBL. 7 REF.Article

DIGIKON: THE DIRECT DIGITAL CONTROL SYSTEM ANALYSIS PROGRAM FOR SHUTTLE.SAXE RK.1976; IN: CONF. DECIS. CONTROL SYMP. ADAPT. PROCESSES. 15 PROC.; CLEARWATER, FLA.; 1976; NEW YORK; INST. ELECTR. ELECTRON. ENG.; DA. 1976; PP. 455-461; BIBL. 8 REF.Conference Paper