Estimation of inertia parameters for gyrostats subject to gravity-gradient torques

Advances in the Astronautical Sciences

Volumn 109 I, Issue , 2002, Pages 113-131

  Peck, Mason A ^a  

^a BOEING COMPANY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; DATA ACQUISITION; MANEUVERABILITY; MATHEMATICAL MODELS; ORBITS; TORQUE;

GYROSTAT;

SPACECRAFT INSTRUMENTS;

EID: 0036063816     PISSN: 00653438     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (21)

1. Mass-properties identification for spacecraft with powerful damping
2. Attitude determination for gyrostats in non-equilibrium spins from infrequent vector observations
3. In-flight estimation of the cassini spacecraft's inertia tensor
4. Estimation of wheel and CMG alignments from on-orbit telemetry
5. A survey of attitude representations
6. A survey of attitude representations
7. Higher order cayley transforms with applications to attitude representations
8. Effect of a rotor on the attitude stability of a satellite in circular orbit
9. On the equilibria of a rigid spacecraft with rotors
10. How to estimate attitude from vector observations
11. Relative equilibria of a rigid satellite in a circular keplerian orbit
12. On-orbit performance of autonomous star trackers
13. IMAGE mission attitude support experiences