Citation: Mg. Matossian, EARTH OBSERVING SYSTEM CONSTELLATION DESIGN OPTIMIZATION THROUGH MIXED-INTEGER PROGRAMMING, Space technology, 16(5-6), 1996, pp. 233-243
Citation: K. Schilling et H. Roth, THE X-RAY SMALL SATELLITE ABRIXAS - MISSION ANALYSIS AND ATTITUDE-CONTROL, Space technology, 16(5-6), 1996, pp. 265-271
Citation: K. Schilling et H. Roth, MISSION ANALYSIS AND ATTITUDE-CONTROL CONCEPTS FOR THE SOLAR OBSERVATION SATELLITE EUVSAT, Space technology, 16(5-6), 1996, pp. 273-279
Citation: Rw. Gundersen et al., A FUZZY-INFERENCE SCHEME FOR FULLY AUTONOMOUS CONTROL OF ROVER CLASS PLANETARY EXPLORATION VEHICLES, Space technology, 16(5-6), 1996, pp. 281-290
Citation: Gt. Yan et al., ATTITUDE DETERMINATION AND CONTROL SUBSYSTEM OF A SMALLSAT FOR MULTIPURPOSE MISSIONS, Space technology, 16(5-6), 1996, pp. 297-301
Citation: Ccj. Ho et Fc. Sheu, AN INNOVATIVE ATTITUDE DETERMINATION USING GPS CARRIER PHASE TRIPLE DIFFERENCE MEASUREMENTS, Space technology, 16(5-6), 1996, pp. 307-316
Citation: Yc. Xie et al., THE ALL-COEFFICIENT ADAPTIVE-CONTROL METHOD AND ITS APPLICATION IN SPACECRAFT ATTITUDE-CONTROL, Space technology, 16(5-6), 1996, pp. 331-336
Citation: Jh. Zeng et al., DYNAMIC CHARACTERISTICS OF SPACECRAFT SLOSHING UNDER GRAVITY-SPINNINGENVIRONMENT, Space technology, 16(5-6), 1996, pp. 337-341
Citation: Dj. Zhang et al., DYNAMIC STIFFENING MODEL OF FLEXIBLE STRUCTURES AND VARIABLE-STRUCTURE CONTROL, Space technology, 16(5-6), 1996, pp. 343-348
Citation: Q. Wang et al., DECENTRALIZED VARIABLE-STRUCTURE CONTROL AND ITS APPLICATION TO FLEXIBLE STRUCTURES, Space technology, 16(5-6), 1996, pp. 349-353
Citation: G. Sachs et M. Dinkelmann, OPTIMIZATION OF 3-DIMENSIONAL RANGE AND ASCENT TRAJECTORIES OF A 2-STAGE HYPERSONIC VEHICLE, Space technology, 16(5-6), 1996, pp. 365-373
Citation: Av. Tishchenko, OPTIMAL MANEUVERS OF A LARGE-SCALE ORBIT TRANSFER VEHICLE WITH LIMITED POWER AND ENERGY-STORAGE, Space technology, 16(5-6), 1996, pp. 375-380
Authors:
MOROZOV YD
PRISNIAKOV VF
PRIVALOV AN
TROFIMENKO AV
GABRINETS VA
GONTAREV YK
Citation: Yd. Morozov et al., SOLAR DYNAMIC RANKINE SPACE POWER-PLANT USING VAPOR-LIQUID METALLIC TECHNIQUES, Space technology, 16(4), 1996, pp. 169-176
Citation: Pn. Keerl, REENTRY - DESCENT AND LANDING TECHNOLOGY AND DEMONSTRATION NEEDS FOR A EUROPEAN UNWINGED VEHICLE, Space technology, 16(4), 1996, pp. 177-185