Asymptotic study of a complete magnetic attitude control cycle providing a single-axis orientation

Ovchinnikov, M Y; Roldugin, D. S.; Penkov, V.I.

doi:10.1016/j.actaastro.2012.03.001

Cited by 29 publications

(9 citation statements)

References 5 publications

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“…We assume no resonance between fast variables rate of change. The damping component (15) averaging result is known [8]. We need to prove that the positional part has no influence on the angular velocity damping, that is…”

Section: Transient Motion Analysismentioning

confidence: 98%

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Three-axis active magnetic attitude control asymptotical study

2015

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Section: Transient Motion Analysismentioning

confidence: 98%

“…We use the averaged (simplified direct dipole) geomagnetic field model following our previous studies [8,9]. The geomagnetic induction vector moves uniformly on the cone side with the doubled orbital angular speed.…”

Section: Geomagnetic Field Modelmentioning

confidence: 99%

Three-axis active magnetic attitude control asymptotical study

2015

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“…Concerning the recent potential investigations in this area, many attentions have been paid on the detumbling of a rigid spacecraft via torque wheel in association with gyroscopic motion [1], where the angular motion of a satellite, which is equipped with the active magnetic attitude control system, is introduced [2]. Attitude stabilization of the satellite through an optimal control strategy is presented [3], while the vehicle system dynamics is reviewed for the purpose of developmenting high-speed trains [4].…”

Section: Related Workmentioning

confidence: 99%

TADC: a new three-axis detumbling mode control approach

Mazinan

Khalaji

2015

Int. J. Dynam. Control

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A new three-axis detumbling mode control approach, namely TADC in the present research, is investigated to deal with a spacecraft, in a short period of time. In a word, the study considers the problem of detumbling by means of system modelling, while the proposed control approach in agreement with the simulation results can be of novelty with respect to the other related potential benchmarks. The approach proposed here plays an important role in this area to adjust angular velocities in the three axes regarding the system under control to be desirable. In some cases, to guarantee the system stability in the process of missions, the whole of angular velocities are to be accurate. In fact, it aims us to organize a number of programmed maneuvers including the orbital, the thermal and so on to be efficient. The idea behind the approach is organized in line with a linear control approach, since the pulse-width pulse-frequency modulator is employed in association with the control allocation to cope with a set of on-off thrusters. Hereinafter, the number of these on-off thrusters may be increased with respect to the investigated control laws to provide overall accurate performance of the spacecraft through the control allocation. The effectiveness of the approach investigated here is finally considered by organizing four scenarios of the experiments and also comparing the outcomes with a number of potential benchmarks.

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“…However, it should be noted that the application of the averaging technique is well developed only for the case where considered systems are fast time-varying. In this case the averaging technique is widely used in a variety of dynamics and control problems [Tikhonov, 2005;Ovchinnikov, Roldugin and Penkov, 2012;Kosjakov, E.A. and Tikhonov, 2015;Kovaleva, 2016;Chikhachev, 2017].…”

Section: Introductionmentioning

confidence: 99%

Rigid body stabilization under time-varying perturbations with zero mean values

Aleksandrov

Тихонов

2018

CAP

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The problem of monoaxial attitude control of a rigid body subjected to nonstationary perturbations is investigated. The control torque consists of a dissipative component and a restoring one. The cases of linear and nonlinear restoring and perturbing torques are analyzed. Two theorems on asymptotic stability of the programmed orientation are proved. The results of a numerical simulation are presented to confirm the conclusions obtained analytically.

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Asymptotic study of a complete magnetic attitude control cycle providing a single-axis orientation

Cited by 29 publications

References 5 publications

Three-axis active magnetic attitude control asymptotical study

Three-axis active magnetic attitude control asymptotical study

TADC: a new three-axis detumbling mode control approach

Rigid body stabilization under time-varying perturbations with zero mean values

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