Pulse modulation for attitude control with thrusters subject to switching restrictions

Aerospace Science and Technology

Volumn 9, Issue 7, 2005, Pages 635-640

  Kienitz, Karl Heinz ^a   Bals, Johann ^a  

^a GERMAN AEROSPACE CENTER DLR   (Germany)

Author keywords

Aerospace control; Attitude control; Pulse modulation; Switching restrictions; Thrusters

Indexed keywords

CONSTRAINT THEORY; DESIGN; MODULATORS; PULSE MODULATION; SPACECRAFT;

AEROSPACE CONTROL; ATTITUDE CONTROL; SWITCHING RESTRICTIONS; THRUSTERS;

CONTROL SYSTEMS;

EID: 26444476985     PISSN: 12709638     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.ast.2005.06.006     Document Type: Article

References (16)

1. N.N. Antropov, G.A. Diakonov, M.N. Kazeev, V.P. Khodnenko, V. Kim, G.A. Popov, A.I. Pokryshkin, Pulsed plasma thrusters for spacecraft attitude and orbit control system, in: Proc. 26th International Propulsion Conference, vol. 2, Kitakyushu, Japan, 1999, pp. 1129-1135
2. G. Avanzini, and G. Matteis Bifurcation analysis of attitude dynamics in rigid spacecraft with switching control logics J. Guidance Control Dynam. 24 2001 953 959
3. A.L. Broadfoot Remote sensing from the space shuttle and space station Adv. Space Res. 19 1997 623 626
4. A.E. Bryson, and Y.-C. Ho Applied Optimal Control: Optimization, Estimation and Control Revised Printing 1975 Hemisphere Publishing Corporation Washington, DC
5. M.O. Hilstad, A Multi-Vehicle Testbed and interface framework for the development and verification of separated spacecraft control algorithms, M.Sc. Thesis, MIT, Cambridge, MA, 2002
6. H. Weidong, and Z. Yulin Rate damping control for small satellite using thruster Acta Astronautica 55 2004 9 13
7. R.E. Martin Atlas II and IIA analyses and environments validation Acta Astronautica 35 1995 771 791
8. R.S. McClelland, Spacecraft attitude control system performance using pulse-width pulse-frequency modulated thrusters, M.Sc. Thesis, Naval Postgraduate School, Monterey, CA, 1994
9. E. Noges, and P.M. Frank Pulsfrequenzmodulierte Regelungssysteme 1975 Oldenbourg München
10. J.G. Reichbach, Micropropulsion system selection for precision formation flying satellites, M.Sc. Thesis, MIT, Cambridge, MA, 2001
11. H. Rom, and A. Gany Thrust control of hydrazine rocket motors by means of pulse width modulation Acta Astronautica 26 1992 313 316
12. G. Song, N.V. Buck, and B.N. Agrawal Spacecraft vibration reduction using pulse-width pulse-frequency modulated input shaper J. Guidance Control Dynam. 22 1999 433 440
13. M.P. Topland, Nonlinear attitude control of the micro-satellite ESEO, M.Sc. Thesis, Norwegian University of Science and Technology, Trondheim, 2004
14. M.P. Topland, J.T. Gravdahl, Nonlinear attitude control of the microsatellite ESEO, in: Proc. 55th International Astronautical Congress, Paper IAC-04-A.P.12, Vancouver, Canada, 2004
15. C. Tournes, Y.B. Shtessel, E. Wells, Upper stage rocket guidance and control using discontinuous reaction control thrusters via sliding modes, in: Proc. 1997 American Control Conference, vol. 4, Albuquerque, NM, 1997, pp. 2547-2551
16. J.E. Vaeth Compatibility of impulse modulation techniques with attitude sensor noise and spacecraft maneuvering IEEE Trans. Automat. Control 10 1965 67 76