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Backstepping based adaptive sliding mode control for spacecraft attitude maneuversBINGLONG CONG; XIANGDONG LIU; ZHEN CHEN et al.Aerospace science and technology (Imprimé). 2013, Vol 30, Num 1, pp 1-7, issn 1270-9638, 7 p.Article

Pulse modulation for attitude control with thrusters subject to switching restrictionsKIENITZ, Karl Heinz; BALS, Johann.Aerospace science and technology. 2005, Vol 9, Num 7, pp 635-640, issn 1270-9638, 6 p.Article

Minimum horizontal rotationsMARCHAL, C.Optimal control applications & methods. 1983, Vol 4, Num 4, pp 357-363, issn 0143-2087Article

Attitude control of a triple inverted pendulumFURUTA, K; OCHIAI, T; ONO, N et al.International Journal of Control. 1984, Vol 39, Num 6, pp 1351-1365, issn 0020-7179Article

Spacecraft attitude control and stabilization: applications of geometric control theory to rigid body modelsCROUCH, P. E.IEEE transactions on automatic control. 1984, Vol 29, Num 4, pp 321-331, issn 0018-9286Article

Exact nonlinear control of large angle rotational maneuversDWYER, T. A. W. III.IEEE transactions on automatic control. 1984, Vol 29, Num 9, pp 769-774, issn 0018-9286Article

Development of a spherical reaction wheel actuator using electromagnetic inductionKIM, Dae-Kwan; HYUNGJOO YOON; KANG, Woo-Yong et al.Aerospace science and technology (Imprimé). 2014, Vol 39, pp 86-94, issn 1270-9638, 9 p.Article

A Gaussian sum filtering approach for phase ambiguity resolution in GPS attitude determinationTURNER, K. J; FARUQI, F. A.International conference on acoustics, speech, and signal processing. 1997, pp 4093-4096, isbn 0-8186-7919-0Conference Paper

A non-linear feedback attitude regulatorSALEHI, S. V; RYAN, E. P.International Journal of Control. 1985, Vol 41, Num 1, pp 281-287, issn 0020-7179Article

Survey of nonlinear attitude estimation methodsCRASSIDIS, John L; LANDIS MARKLEY, F; YANG CHENG et al.Journal of guidance, control, and dynamics. 2007, Vol 30, Num 1, pp 12-28, issn 0731-5090, 17 p.Article

Analysis and design of air-cored halbach array permanent magnet BDCMZHAO, Jianhui; XU, Yanliang.Proceedings of SPIE, the International Society for Optical Engineering. 2006, issn 0277-786X, isbn 0-8194-6452-X, Vol. 1, 63571G.1-63571G.6Conference Paper

Equivalency between strapdown inertial navigation coning and sculling integrals/algorithmsROSCOE, Kelly M.Journal of guidance, control, and dynamics. 2001, Vol 24, Num 2, pp 201-205, issn 0731-5090Article

Vibration suppression of flexible spacecraft during attitude maneuversQINGLEI HU; GUANGFU MA.Journal of guidance, control, and dynamics. 2005, Vol 28, Num 2, pp 377-380, issn 0731-5090, 4 p.Article

Approaches to making the optical systems of the adaptive star trackers for attitude control of space vehiclesKOLOSOV, M. P; EISOUROVICH, A. L.SPIE proceedings series. 1997, pp 339-346, isbn 0-8194-2501-XConference Paper

A signed switching time bang-bang attitude control law for fine pointing of flexible spacecraftDODDS, S. J; WILLIAMSON, S. E.International Journal of Control. 1984, Vol 40, Num 4, pp 795-811, issn 0020-7179Article

Attitude Dynamics of Rigid Bodies in the Vicinity of Lagrangian PointsWONG, Brian; PATIL, Rakesh; MISRA, Arun et al.Journal of guidance, control, and dynamics. 2008, Vol 31, Num 1, pp 252-256, issn 0731-5090, 5 p.Article

A predicted signed switching time high precision satellite attitude control lawDODDS, S. J.International Journal of Control. 1984, Vol 39, Num 5, pp 1051-1061, issn 0020-7179Article

Inverse optimal and robust nonlinear attitude control of rigid spacecraftPARK, Yonmook.Aerospace science and technology (Imprimé). 2013, Vol 28, Num 1, pp 257-265, issn 1270-9638, 9 p.Article

Attitude control of magnetically actuated satellites with an uneven inertia distributionWOOD, Mark; CHEN, Wen-Hua.Aerospace science and technology (Imprimé). 2013, Vol 25, Num 1, pp 29-39, issn 1270-9638, 11 p.Article

ATTITUDE CONTROL OF THE SME SATELLITE: A FLIGHT EXPERIENCESTEWART KD; COWLEY JR; LAWRENCE GM et al.1982; ADV. ASTRONAUT. SCI.; ISSN 0065-3438; USA; DA. 1982; VOL. 48; PP. 507-536; BIBL. 4 REF.Conference Paper

AUTONOMOUS ATTITUDE CONTROLWILLIAMSON RK; MANKE GM; GILLEY GC et al.1982; ADV. ASTRONAUT. SCI.; ISSN 0065-3438; USA; DA. 1982; VOL. 48; PP. 383-396; BIBL. 6 REF.Conference Paper

THE ATTITUDE DETERMINATION AND CONTROL SYSTEM FOR THE SOLAR MESOPHERE EXPLORER SATELLITESTEWART KD.1981; GUIDANCE AND CONTROL CONFERENCE/1981/ALBUQUERQUE NM; USA; NEW-YORK: AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS; DA. 1981; PP. 234-240; BIBL. 4 REF.Conference Paper

A BASIC ATTITUDE INSTABILITY OF SPACECRAFT WITH IMPERFECT MOMENTUM WHEELS = UNE INSTABILITE D'ATTITUDE FONDAMENTALE D'UN VEHICULE SPATIAL AVEC DES ROUES MOTRICES IMPARFAITESTONKIN SW.1980; AUTOMATICA (OXF.); ISSN 0005-1098; GBR; DA. 1980; VOL. 16; NO 4; PP. 415-418; BIBL. 2 REF.Article

TWO DECADES OF SPACECRAFT ATTITUDE CONTROLROBERSON RE.1978; AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS AEROSPACE SCIENCES MEETING. 16/1978/HUNTSVILLE AL; USA; NEW YORK: AIAA; DA. 1978; 78-7; 8 P.; BIBL. 30 REF.Conference Paper

SMM ATTITUDE CONTROL RECOVERYHOFFMAN HC; DONOHUE JH; FLATLEY TW et al.1981; GUIDANCE AND CONTROL CONFERENCE/1981/ALBUQUERQUE NM; USA; NEW-YORK: AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS; DA. 1981; PP. 84-90Conference Paper

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