DOI

The problem of Lorentz stabilization of a satellite in the orbital coordinate system on an orbit of small inclination under conditions of a disturbing gravitational torque is studied. To solve this problem, which is characterized by incomplete control, the averaging technique for differential equations is developed. An original construction of a Lyapunov function is used.

Original languageEnglish
Title of host publicationProceedings of 2020 15th International Conference on Stability and Oscillations of Nonlinear Control Systems (Pyatnitskiy's Conference), STAB 2020
EditorsValentin N. Tkhai
PublisherInstitute of Electrical and Electronics Engineers Inc.
ISBN (Electronic)9781728167053
ISBN (Print)9781728167053
DOIs
StatePublished - Jun 2020
Event15th International Conference on Stability and Oscillations of Nonlinear Control Systems (Pyatnitskiy's Conference) (STAB): Pyatnitskiy's Conference - ИПУ РАН, Москва, Russian Federation
Duration: 2 Jun 2020 → 5 Jun 2020
Conference number: 15

Publication series

NameProceedings of 2020 15th International Conference on Stability and Oscillations of Nonlinear Control Systems (Pyatnitskiy's Conference), STAB 2020

Conference

Conference15th International Conference on Stability and Oscillations of Nonlinear Control Systems (Pyatnitskiy's Conference) (STAB)
Abbreviated titleSTAB 2020
Country/TerritoryRussian Federation
CityМосква
Period2/06/20 → 5/06/20

    Scopus subject areas

  • Control and Systems Engineering
  • Mechanical Engineering
  • Control and Optimization

    Research areas

  • averaging technique, Lyapunov function, satellite, stabilization

ID: 64666702