The high accuracy attitude control of a one-dimensionally rotating spacecraft, equipped with a noisy attitude sensor and a noisy reaction wheel for attitude control, acted upon by a noisy external disturbing torque, and required to execute a desired or target attitude motion is discussed. Stochastic stability properties of the closed loop system are investigated, both analytically and geometrically. The results obtained are compared with those of other modern attitude control designs as well as with those of classical attitude control designs.
Survey of Modern Control and Observation Theory for Disturbed, Target Following Aerospace Systems. Part 2: Stochastic Performance and Spacecraft Application
1978
111 pages
Report
Keine Angabe
Englisch