Guidance and Robust Gyromoment Attitude Control of Agile Flexible Remote Sensing Spacecraft

Somov, Yevgeny; Butyrin, Sergey; Somov, Sergey; Anshakov, G.P.

doi:10.3182/20070625-5-fr-2916.00091

Cited by 8 publications

(2 citation statements)

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“…Vectors ω(t), ε(t) andε(t) ≡ v(t) are analytically defined by recurrent algorithm [16] using functions ϕ k (t) and their derivatives.…”

Section: Optimizing a Rotation Maneuvermentioning

confidence: 99%

“…Increased requirements to such information satellites (lifetime up to 10 years, exactness of spatial rotation maneuvers with effective damping the SC flexible structure oscillations, robustness, fault-tolerance as well as to reasonable mass, size and energy characteristics) have motivated intensive development the gyro moment clusters (GMCs) based on excessive number of gyrodines (GDs) -single-gimbal control moment gyros. Mathematical aspects of the SC nonlinear gyromoment control were represented in a number of research works [1,2] et al including the authors' papers [3][4][5][6][7][8][9][10][11][12][13][14][15][16][17][18]. The paper suggests new results on attitude guidance and nonlinear robust gyromoment attitude control of the agile observation spacecraft.…”

Section: Introductionmentioning

confidence: 99%

See 1 more Smart Citation

Methods for attitude guidance and precise robust gyromoment control of large-scale agile observation spacecraft

Somov¹,

Butyrin²,

Somov³

2012

AIP Conference Proceedings

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Articles you may be interested inCalibration and alignment of strapped-down astro-inertial system for attitude determination of large-scale information spacecraft AIP Conf. Proc. 1493, 949 (2012); 10.1063/1.4765601Spacecraft attitude pulse-width control at initial, service and emergency modes AIP Conf.Abstract. Problems on guidance and robust gyromoment attitude control of agile information satellite for remote sensing the Earth surface are considered. Elaborated methods for dynamic research of the spacecraft programmed angular motion at principle modes under external and parametric disturbances, partial discrete measurement of the state and digital control of the gyro moment cluster by the excessive gyrodine schemes, are presented.

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“…Vectors ω(t), ε(t) andε(t) ≡ v(t) are analytically defined by recurrent algorithm [16] using functions ϕ k (t) and their derivatives.…”

Section: Optimizing a Rotation Maneuvermentioning

confidence: 99%