431
Views
29
CrossRef citations to date
0
Altmetric
Original Articles

Time-optimal reorientation for rigid satellite with reaction wheels

, , &
Pages 1452-1463 | Received 01 Dec 2011, Accepted 23 Apr 2012, Published online: 18 May 2012

References

  • Ahmed , J , Coppola , VT and Bernstein , DS . 1998 . Adaptive Asymptotic Tracking of Spacecraft Attitude Motion with Inertia Matrix Identification . Journal of Guidance Control and Dynamics , 21 : 684 – 691 .
  • Bao , X and Junkins , JL . 2009 . New Results for Time-optimal Three-axis Reorientation of a Rigid Spacecraft . Journal of Guidance Control and Dynamics , 32 : 1071 – 1076 .
  • Bilimoria , KD and Wie , B . 1993 . Time-optimal Three-axis Reorientation of a Rigid Spacecraft . Journal of Guidance Control and Dynamics , 16 : 446 – 452 .
  • Bošković , JD , Li , S and Mehra. , RK . 2004 . Robust Tracking Control Design for Spacecraft under Control Input Saturation . Journal of Guidance Control and Dynamics , 27 : 627 – 633 .
  • Boyarko , GA , Romano , M and Yakimenko , OA . 2011 . Time-optimal Reorientation of a Spacecraft using an Inverse Dynamics Optimization Method . Journal of Guidance Control and Dynamics , 34 : 1197 – 1208 .
  • Elnagar , G , Kazemi , MA and Razzaghi , M . 1995 . The Pseudospectral Legendre Method for Discretizing Optimal Control Problems . IEEE Transaction on Automatic Control , 40 : 1793 – 1796 .
  • Fleming , A , Sekhavat , P and Ross , IM . 2010 . Minimum-time Reorientation of a Rigid Body . Journal of Guidance Control and Dynamics , 33 : 160 – 170 .
  • Gennaro , SD , Monaco , S and Normand-Cyrot , D . 1999 . Nonlinear Digital Scheme for Attitude Tracking . Journal of Guidance Control and Dynamics , 22 : 467 – 477 .
  • Holmström , K . Göran, A.O., and Edvall, M.M. (2006), “Users Guide for TOMLAB/SNOPT,” Mälardalen University, Department of Mathematics and Physics: Västerås, Sweden
  • Jan , Y and Chiou , J . 2004 . Minimum-time Spacecraft Maneuver using Sliding-mode Control . ACTA Astronautica , 54 : 69 – 75 .
  • Lai , LC , Yang , CC and Wu , CJ . 2007 . Time-optimal Maneuvering Control of a Rigid Spacecraft . ACTA Astronautica , 60 : 791 – 800 .
  • Levskii , MV . 2009 . The Problem of the Time-optimal Control of Spacecraft Reorientation . Journal of Applied Mathematics and Mechanics , 73 : 16 – 25 .
  • Liu , S and Singh , T . 1996 . Fuel/Time Optimal Control of Spacecraft Maneuvers . Journal of Guidance Control and Dynamics , 20 : 394 – 397 .
  • Melton , RG . (2010), ‘Boundary Points and Arcs in Constrained, Time-optimal Satellite Reorientation Maneuvers’, in AIAA/AAS Astrodynamics Specialist Conference, 2–5 August 2010, Toronto, ON, Canada, pp. 1–16
  • Ross , IM . and Fahroo, F. (2001), ‘Convergence of Pseudospectral Discretizations of Optimal Control Problems’, in Proceedings of the 40th IEEE Conference on Decision and Control, December 2001, Orlando, FL, USA, pp. 3175–3177
  • Shen , H and Tsiotras , P . 1999 . Time-optimal Control of Axisymmetric Rigid Spacecraft using Two Controls . Journal of Guidance Control and Dynamics , 22 : 682 – 694 .
  • Sharma , R and Tewari , A . 2004 . Optimal Nonlinear Tracking of Spacecraft Attitude Maneuvers . IEEE Transactions on Control Systems Technology , 12 : 677 – 682 .
  • Wen , JT and Kreutz-Delgado , K . 1991 . The Attitude Control Problem . IEEE Transactions on Automatic Control , 36 : 1148 – 1162 .
  • Wie , B and Weiss , H . 1989 . Quaternion Feedback Regulator for Spacecraft Eigenaxis Rotations . Journal of Guidance Control and Dynamics , 12 : 375 – 380 .
  • Wu , B , Wang , D , Poh , EK and Xu , G . 2009 . Nonlinear Optimization of Low-thrust Trajectory for Satellite Formation: Legendre Pseudospectral Approach . Journal of Guidance Control and Dynamics , 32 : 1371 – 1381 .
  • Yang , CC , Lai , LC and Wu , CJ . 2007 . Minimal Energy Maneuvering Control of a Rigid Spacecraft with Momentum Transfer . Journal of the Franklin Institude – Engineering and Applied Mathematics , 344 : 991 – 1005 .
  • Zheng , J , Banks , SP and Alleyne , H . 2005 . Optimal Attitude Control for Three-axis Stabilized Flexible Spacecraft . ACTA Astronautica , 56 : 519 – 528 .

Reprints and Corporate Permissions

Please note: Selecting permissions does not provide access to the full text of the article, please see our help page How do I view content?

To request a reprint or corporate permissions for this article, please click on the relevant link below:

Academic Permissions

Please note: Selecting permissions does not provide access to the full text of the article, please see our help page How do I view content?

Obtain permissions instantly via Rightslink by clicking on the button below:

If you are unable to obtain permissions via Rightslink, please complete and submit this Permissions form. For more information, please visit our Permissions help page.