Mixed H2/H⊥ state-feedback design for microsatellite attitude control

Control Engineering Practice

Volumn 10, Issue 9, 2002, Pages 951-970

  Yang, Ciann Dong ^a   Sun, Yun Ping ^b  

^a NATIONAL CHENG KUNG UNIVERSITY   (Taiwan)

^b CHENG SHIU UNIVERSITY   (Taiwan)

Author keywords

Attitude control; Linear matrix inequality method; Microsatellite; Mixed H2 H control

Indexed keywords

METHOD OF MOMENTS; ROBUSTNESS (CONTROL SYSTEMS); STABILITY;

MICROSATELLITES;

FEEDBACK;

DESIGN; POSITIONING CONTROL SYSTEM; SATELLITE;

EID: 0036747016     PISSN: 09670661     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0967-0661(02)00049-7     Document Type: Article

References (49)

1. SAC-A attitude control design
2. All stellar attitude estimation using A ball CT-633 star tracker
3. LQG control with an H∞ performance bound: A Riccati equation approach
4. High fidelity mathematical modeling of reaction wheel performance
5. Linear matrix inequalities in system and control theory
6. The DLR small satellite mission BIRD
7. 2/H∞ attitude control of spacecraft
8. H∞ design with pole placement constraints: An LMI approach
9. Direct connection between time-domain performance and frequency-domain characteristics
10. Preliminary design of the attitude control system of a microsatellite for earth observation
11. Performance of the MSX guidance and control system
12. Robust, fragile, or optimal?
13. 2/H∞ control: A convex optimization approach
14. Precision pointing for the Pluto mission spacecraft
15. Nanosatellites and micro systems technology-Capabilities, limitations and applications
16. Design of H∞ attitude controllers for spacecraft using a magnetically suspended momentum wheel
17. An approach to the design and implementation of spacecraft attitude control systems
18. SMART attitude acquisition and control
19. H∞ optimization with time-domain constraints
20. Pre-project of microsatellite for remote sensing and climate data collection
21. 2/H∞ control
22. Multiobjective output-feedback control via LMI optimization
23. Spacecraft nonlinear control
24. Ultra-precision attitude control of a large low-orbital space telescope
25. Classical and robust H∞ control redesign for the Hubble space telescope
26. Robust stabilization of the space station in the presence of inertia matrix uncertainty
27. Attitude determination and control for the global imaging system 2000
28. A magnetic attitude control system for sun pointing satellites
29. Comparative study of various control methods for attitude control of a LEO satellite
30. On the input-output stability of nonlinear time-varying feedback systems, Part I: Conditions derived using concepts of loop gain, conicity and positivity
31. On the input-output stability of nonlinear time-varying feedback systems, Part II: Conditions involving circles in the frequency plane and sector nonlinearities
32. On-orbit performance of the transition region and coronal explorer (TRACE) attitude control system