Skip to content

Latest commit

 

History

History
16 lines (15 loc) · 463 Bytes

README.md

File metadata and controls

16 lines (15 loc) · 463 Bytes

adcs_jm

Attitude determination and control system of a CubeSat
Attitude determination is provided by Extended Kalman Filter and Multiplicative Kalman Filter

Attitude control algorithms -

  1. B-dot
  2. Linear quadratic
    • Constant gain
    • Periodic
  3. Model predictive

For live demostration run main_simulation.m. For deep precomputation run main_figures