Synthesis of control algorithms of the spacecraft spatial reori-entation with the use of dynamic equations of a solid body rotational mo-tion in Rodrigo–Hamilton parameters

Ähnliche Einträge

• Synthesis of time-optimal three-dimensional rotation of spacecraft using rotational motion of equation of rigid body at Rodrigues–Hamilton parameters
  von: N. V. Efimenko
  Veröffentlicht: (2017)
• Determination of the parameters of the angular motion of the spacecraft from the information of the star sensor using the dynamic equation of the solid body rotation in the Rodrig–Hamilton parameters
  von: N. V. Efimenko, et al.
  Veröffentlicht: (2018)
• Mathematical Model of an the Angular Motion of a Solid Body in the Parameters of the Rodrig-Hamilton and its use in the Tasks of Control Spacecraft Orientation
  von: N. V. Efimenko
  Veröffentlicht: (2018)
• Mathematical Model of the Angular Motion of a Spacecraft in the Rodrig-Hamilton Parameters and Its Properties
  von: N. V. Efimenko
  Veröffentlicht: (2018)
• Algorithms of the attitude matching of star tracker and camera of the spacecraft
  von: A. I. Tkachenko
  Veröffentlicht: (2015)