ACOSS-16 (Active Control of Space Structures)
Final technical rept. May 1981-Jul 1982
HONEYWELL SYSTEMS AND RESEARCH CENTER MINNEAPOLIS MN
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The objective of this effort is to develop, design and analyze techniques that can be used to meet future line of sight and jitter control requirements of large space structures that have onboard disturbances. This effort studied parameter identification on a representative large space structure and the impact of on-orbit identification on the design of a disturbance controller for the spacecraft.
- Numerical Mathematics
- Unmanned Spacecraft