On satellite electrodynamic attitude stabilization

Electrodynamic stabilization of artificial earth satellites in the König coordinate system

“…The initial conditions for the AES motion are Here, ϕ, ψ, and θ are the "aircraft" angles having the same sense as in [14,16]. The control parameter values satisfying inequalities (5.9) were taken from (5.13).…”

“…The programmed motion can be stabilized by (following the technique used in [14] and [16]) taking the laws of change of each of the parameters and to be the sum of two terms:…”

“…The proposed control method can be imple mented in practice without fundamental difficulties. An example of the numerical simulation of the AES's stabilization with similar control parameters but in the rotating coordinate system was considered in [16].…”

“…The electrodynamic method of AES stabilization is based on the simultaneous use of the Lorentz and magnetic control torques [14][15][16]. These studies proposed a principle for the creation of restoring and damping components of control torques, analyzed the possibilities to optimize the control aimed at reducing the energy consumption.…”

On electrodynamical compensation of a torque disturbing satellite orientation

“…Later the concept of the electrodynamic attitude control system was improved in [2] and further used for solving the problems of three-axis stabilization of a satellite in the orbital coordinate system (see [3] and papers cited therein), monoaxial stabilization of a satellite in the orbital coordinate system [4], stabilization of a satellite in biaxial spin mode [5], three-axis stabilization of a satellite in the König coordinate system [6].…”