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Results: 1-13 |
Results: 13
TOUCH POINTS IN OPTIMAL ASCENT TRAJECTORIES WITH FIRST-ORDER STATE INEQUALITY CONSTRAINTS
Authors: PARK SY VADALI SR
Citation: Sy. Park et Sr. Vadali, TOUCH POINTS IN OPTIMAL ASCENT TRAJECTORIES WITH FIRST-ORDER STATE INEQUALITY CONSTRAINTS, Journal of guidance, control, and dynamics, 21(4), 1998, pp. 603-610
AN INVERSE-FREE TECHNIQUE FOR ATTITUDE-CONTROL OF SPACECRAFT USING CMGS
Authors: KRISHNAN S VADALI SR
Citation: S. Krishnan et Sr. Vadali, AN INVERSE-FREE TECHNIQUE FOR ATTITUDE-CONTROL OF SPACECRAFT USING CMGS, Acta astronautica, 39(6), 1996, pp. 431-438
SUBOPTIMAL COMMAND GENERATION FOR CONTROL MOMENT GYROSCOPES AND FEEDBACK-CONTROL OF SPACECRAFT
Authors: VADALI SR KRISHNAN S
Citation: Sr. Vadali et S. Krishnan, SUBOPTIMAL COMMAND GENERATION FOR CONTROL MOMENT GYROSCOPES AND FEEDBACK-CONTROL OF SPACECRAFT, Journal of guidance, control, and dynamics, 18(6), 1995, pp. 1350-1354
NEAR-MINIMUM-TIME MANEUVERS OF LARGE STRUCTURES - THEORY AND EXPERIMENTS
Authors: VADALI SR CARTER MT SINGH T ABHYANKAR NS
Citation: Sr. Vadali et al., NEAR-MINIMUM-TIME MANEUVERS OF LARGE STRUCTURES - THEORY AND EXPERIMENTS, Journal of guidance, control, and dynamics, 18(6), 1995, pp. 1380-1385
MODELING ISSUES RELATED TO RETRIEVAL OF FLEXIBLE TETHERED SATELLITE SYSTEMS
Authors: KIM E VADALI SR
Citation: E. Kim et Sr. Vadali, MODELING ISSUES RELATED TO RETRIEVAL OF FLEXIBLE TETHERED SATELLITE SYSTEMS, Journal of guidance, control, and dynamics, 18(5), 1995, pp. 1169-1176
NEAR-OPTIMAL 3-DIMENSIONAL ROTATIONAL MANEUVERS OF SPACECRAFT USING MANIPULATOR ARMS
Authors: KRISHNAN S VADALI SR
Citation: S. Krishnan et Sr. Vadali, NEAR-OPTIMAL 3-DIMENSIONAL ROTATIONAL MANEUVERS OF SPACECRAFT USING MANIPULATOR ARMS, Journal of guidance, control, and dynamics, 18(4), 1995, pp. 932-934
TRAJECTORY OPTIMIZATION USING PARALLEL SHOOTING METHOD ON PARALLEL COMPUTER
Authors: WIRTHMAN DJ PARK SY VADALI SR
Citation: Dj. Wirthman et al., TRAJECTORY OPTIMIZATION USING PARALLEL SHOOTING METHOD ON PARALLEL COMPUTER, Journal of guidance, control, and dynamics, 18(2), 1995, pp. 377-379
ROBUST TIME-DELAY CONTROL OF MULTIMODE SYSTEMS
Authors: SINGH T VADALI SR
Citation: T. Singh et Sr. Vadali, ROBUST TIME-DELAY CONTROL OF MULTIMODE SYSTEMS, International Journal of Control, 62(6), 1995, pp. 1319-1339
ROBUST TIME-OPTIMAL CONTROL - FREQUENCY-DOMAIN APPROACH
Authors: SINGH T VADALI SR
Citation: T. Singh et Sr. Vadali, ROBUST TIME-OPTIMAL CONTROL - FREQUENCY-DOMAIN APPROACH, Journal of guidance, control, and dynamics, 17(2), 1994, pp. 346-353
COMPUTATION OF NEAR-MINIMUM-TIME MANEUVERS OF FLEXIBLE STRUCTURES BY PARAMETER OPTIMIZATION
Authors: VADALI SR SINGH T CARTER T
Citation: Sr. Vadali et al., COMPUTATION OF NEAR-MINIMUM-TIME MANEUVERS OF FLEXIBLE STRUCTURES BY PARAMETER OPTIMIZATION, Journal of guidance, control, and dynamics, 17(2), 1994, pp. 354-360
OPTIMAL OPEN-LOOP AND FEEDBACK-CONTROL USING SINGLE GIMBAL CONTROL MOMENT GYROSCOPES
Authors: HOELSCHER BR VADALI SR
Citation: Br. Hoelscher et Sr. Vadali, OPTIMAL OPEN-LOOP AND FEEDBACK-CONTROL USING SINGLE GIMBAL CONTROL MOMENT GYROSCOPES, The Journal of the astronautical sciences, 42(2), 1994, pp. 189-206
INPUT-SHAPED CONTROL OF 3-DIMENSIONAL MANEUVERS OF FLEXIBLE SPACECRAFT
Authors: SINGH T VADALI SR
Citation: T. Singh et Sr. Vadali, INPUT-SHAPED CONTROL OF 3-DIMENSIONAL MANEUVERS OF FLEXIBLE SPACECRAFT, Journal of guidance, control, and dynamics, 16(6), 1993, pp. 1061-1068
QUASI-CLOSED-FORM SOLUTION TO THE TIME-OPTIMAL RIGID SPACECRAFT REORIENTATION PROBLEM
Authors: BYERS RM VADALI SR
Citation: Rm. Byers et Sr. Vadali, QUASI-CLOSED-FORM SOLUTION TO THE TIME-OPTIMAL RIGID SPACECRAFT REORIENTATION PROBLEM, Journal of guidance, control, and dynamics, 16(3), 1993, pp. 453-461
Risultati: 1-13 |