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Results: 1-14 |
Results: 14
MINIMAL-PARAMETER ATTITUDE MATRIX ESTIMATION FROM VECTOR OBSERVATIONS
Authors: OSHMAN Y MARKLEY FL
Citation: Y. Oshman et Fl. Markley, MINIMAL-PARAMETER ATTITUDE MATRIX ESTIMATION FROM VECTOR OBSERVATIONS, Journal of guidance, control, and dynamics, 21(4), 1998, pp. 595-602
UNCONSTRAINED OPTIMAL TRANSFORMATION MATRIX
Authors: MARKLEY FL BARITZHACK IY
Citation: Fl. Markley et Iy. Baritzhack, UNCONSTRAINED OPTIMAL TRANSFORMATION MATRIX, IEEE transactions on aerospace and electronic systems, 34(1), 1998, pp. 338-340
NONLINEAR PREDICTIVE CONTROL OF SPACECRAFT
Authors: CRASSIDIS JL MARKLEY FL ANTHONY TC ANDREWS SF
Citation: Jl. Crassidis et al., NONLINEAR PREDICTIVE CONTROL OF SPACECRAFT, Journal of guidance, control, and dynamics, 20(6), 1997, pp. 1096-1103
MINIMUM MODEL ERROR APPROACH FOR ATTITUDE ESTIMATION
Authors: CRASSIDIS JL MARKLEY FL
Citation: Jl. Crassidis et Fl. Markley, MINIMUM MODEL ERROR APPROACH FOR ATTITUDE ESTIMATION, Journal of guidance, control, and dynamics, 20(6), 1997, pp. 1241-1247
NEW ALGORITHM FOR ATTITUDE DETERMINATION USING GLOBAL POSITIONING SYSTEM SIGNALS
Authors: CRASSIDIS JL MARKLEY FL
Citation: Jl. Crassidis et Fl. Markley, NEW ALGORITHM FOR ATTITUDE DETERMINATION USING GLOBAL POSITIONING SYSTEM SIGNALS, Journal of guidance, control, and dynamics, 20(5), 1997, pp. 891-896
PREDICTIVE FILTERING FOR ATTITUDE ESTIMATION WITHOUT RATE SENSORS
Authors: CRASSIDIS JL MARKLEY FL
Citation: Jl. Crassidis et Fl. Markley, PREDICTIVE FILTERING FOR ATTITUDE ESTIMATION WITHOUT RATE SENSORS, Journal of guidance, control, and dynamics, 20(3), 1997, pp. 522-527
PREDICTIVE FILTERING FOR NONLINEAR-SYSTEMS
Authors: CRASSIDIS JL MARKLEY FL
Citation: Jl. Crassidis et Fl. Markley, PREDICTIVE FILTERING FOR NONLINEAR-SYSTEMS, Journal of guidance, control, and dynamics, 20(3), 1997, pp. 566-572
SLIDING MODE CONTROL USING MODIFIED RODRIGUES PARAMETERS
Authors: CRASSIDIS JL MARKLEY FL
Citation: Jl. Crassidis et Fl. Markley, SLIDING MODE CONTROL USING MODIFIED RODRIGUES PARAMETERS, Journal of guidance, control, and dynamics, 19(6), 1996, pp. 1381-1383
ATTITUDE-CONTROL SYSTEM CONCEPTUAL DESIGN FOR GEOSTATIONARY OPERATIONAL ENVIRONMENTAL SATELLITE SPACECRAFT SERIES
Authors: MARKLEY FL BAUER FH DEILY JJ FEMIANO MD
Citation: Fl. Markley et al., ATTITUDE-CONTROL SYSTEM CONCEPTUAL DESIGN FOR GEOSTATIONARY OPERATIONAL ENVIRONMENTAL SATELLITE SPACECRAFT SERIES, Journal of guidance, control, and dynamics, 18(2), 1995, pp. 247-255
AUTONOMOUS SPACECRAFT GYRO FAILURE-DETECTION BASED ON CONSERVATION OFANGULAR-MOMENTUM
Authors: MARKLEY FL KENNEDY KR NELSON JD MOY EW
Citation: Fl. Markley et al., AUTONOMOUS SPACECRAFT GYRO FAILURE-DETECTION BASED ON CONSERVATION OFANGULAR-MOMENTUM, Journal of guidance, control, and dynamics, 17(6), 1994, pp. 1385-1387
ZERO-GYRO SAFEMODE CONTROLLER FOR THE HUBBLE-SPACE-TELESCOPE
Authors: MARKLEY FL NELSON JD
Citation: Fl. Markley et Jd. Nelson, ZERO-GYRO SAFEMODE CONTROLLER FOR THE HUBBLE-SPACE-TELESCOPE, Journal of guidance, control, and dynamics, 17(4), 1994, pp. 815-822
NEW QUATERNION ATTITUDE ESTIMATION METHOD
Authors: MARKLEY FL
Citation: Fl. Markley, NEW QUATERNION ATTITUDE ESTIMATION METHOD, Journal of guidance, control, and dynamics, 17(2), 1994, pp. 407-409
NEW DYNAMIC VARIABLES FOR MOMENTUM-BIAS SPACECRAFT
Authors: MARKLEY FL
Citation: Fl. Markley, NEW DYNAMIC VARIABLES FOR MOMENTUM-BIAS SPACECRAFT, The Journal of the astronautical sciences, 41(4), 1993, pp. 557-567
ATTITUDE DETERMINATION USING VECTOR OBSERVATIONS - A FAST OPTIMAL MATRIX ALGORITHM
Authors: MARKLEY FL
Citation: Fl. Markley, ATTITUDE DETERMINATION USING VECTOR OBSERVATIONS - A FAST OPTIMAL MATRIX ALGORITHM, The Journal of the astronautical sciences, 41(2), 1993, pp. 261-280
Risultati: 1-14 |