References
- Wie, B., and Barba, P. M., "Quaternion Feedback for Spacecraft Large Angle Maneuvers," Journal of Guidance, Control and Dynamics, Vol. 8, No. 3, 1985, pp. 360-365. https://doi.org/10.2514/3.19988
- Wie, B., Weiss, H., and Arapostathis, A., "Quaternion Feedback Regulator for Spacecraft Eigenaxis Rotations," Journal of Guidance, Control and Dynamics, Vol. 12, No. 3, 1989, pp. 375-380. https://doi.org/10.2514/3.20418
- Steyn, W. H., "Near-Minimum-Time Eigenaxis Rotation Maneuvers Using Reaction Wheels," Journal of Guidance, Control and Dynamics, Vol. 18, No. 5, 1995, pp. 1184-1189. https://doi.org/10.2514/3.21523
- Wallsgrove, R. J., and Akella, M. R., "Globally Stabilizing Saturated Attitude Control in the Presence of Bounded Unknown Disturbances," Journal of Guidance, Control and Dynamics, Vol. 28, No. 5, 2005, pp. 957-963. https://doi.org/10.2514/1.9980
- Mayhew, C. G., Sanfelice, R. G., and Teel, A. R., "Quaternion-Based Hybrid Control for Robust Global Attitude Tracking," IEEE Transactions on Automatic Control, Vol. 56, No. 11, 2011, pp. 2555-2566. https://doi.org/10.1109/TAC.2011.2108490
- Hu, Q., Tan, X., and Akella, M. R., "Finite-Time Fault-Tolerant Spacecraft Attitude Control with Torque Saturation," Journal of Guidance, Control and Dynamics, Vol. 40, No. 10, 2017, pp. 2524-2537. https://doi.org/10.2514/1.G002191
- Yoon, H., Choi, J. H., Chugn, Y., and Bang, H., "Practical Approach for Quick Attitude Maneuver of Spacecraft with Actuator Saturation," 63th International Astronautical Congress, Italy, 2012, IAC-12-C1.9.2.
- Liu, Q., and Wie, B., "Robust Time-Optimal Control of Uncertain Flexible Spacecraft," Journal of Guidance, Control and Dynamics, Vol. 15, No. 3, 1992, pp. 597-604. https://doi.org/10.2514/3.20880
- Bilimoria, K. D., and Wie, B., "Time-Optimal Three-Axis Reorientation of a Rigid Spacecraft," Journal of Guidance, Control and Dynamics, Vol. 16, No. 3, 1993, pp. 446-452. https://doi.org/10.2514/3.21030
- Adams, D., Bruno, D., Shah, P., and Keller, B. S., "Precision Control, Knowledge and Orbit Determination on a Small Spacecraft Bus: The OrbView-4 Attitude Control System," 12th AIAA/USU Conference on Small Satellites, USA, 1998, SSC98-IX-3.
- Roser, X., Silvestrin, P., Labandibar, J. Y., and Jubineau, F., "Agile AOCS Definition for an Optical Earth Observation Mission: LSPIM," 4th International Conference on Spacecraft Guidance, Navigation and control Systems, Netherlands, 1999.
- Lafontaine, J. D., Buijs, J., Vuilleumier, P., Braembussche, P. V. D., "Development of the PROBA Attitude Control and Navigation Software," 4th International Conference on Spacecraft Guidance, Navigation and control Systems, Netherlands, 1999.
- Macala, G. A., "Design of the Reaction Wheel Attitude Control System for the Cassini Spacecraft," AAS/AIAA Space Flight Mechanics Meeting, Pasadena, CA, USA, 2002, AAS-02-121.
- Thieuw, A., and Marcille, H., "Pleiades-HR CMGs-Based Attitude Control System Design, Development Status and Performances," 17th IFAC Symposium on Automatic Control in Space, France, 2007.
- Vadali, S. R., and Junkins, J., "Optimal Open-Loop and Stable Feedback Control of Rigid Spacecraft Attitude Maneuvers," The Journal of the Astronautical Sciences, Vol. 32, No. 2, 1984, pp. 105-122.
- Markley, F. L., Reynolds, R. G., Liu, F. X., and Lebsock, K. L., "Maximum Torque and Momentum Envelopes for Reaction-Wheel Arrays," Journal of Guidance, Control and Dynamics, Vol. 33, No. 5, 2010, pp. 1606-1614. https://doi.org/10.2514/1.47235
- Carrara, V., Sinqueira, R. H., and Oliveira, D., "Speed and Current Control Mode Strategy Comparison in Satellite Attitude Control with Reaction Wheels," ABCM Symposium Series in Mechatronics, Vol. 5, 2012, pp. 533-542.
- Carrara, V., and Kuga, H. K., "Torque and Speed Control Loops of a Reaction Wheel," 11th International Conference on Vibration Problems, Portugal, Sep. 2013.
- Mok, S.-H., Bang, H., and Kim, H.-S., "Analytical Solution for Attitude Command Generation of Agile Spacecraft," Journal of the Korean Society for Aeronautical and Space Sciences, Vol. 46, No. 8, 2018, pp. 639-651. https://doi.org/10.5139/JKSAS.2018.46.8.639
- Yoon, H., Seo, H. H., and Choi, H.-T., "Optimal Uses of Reaction Wheels in the Pyramid Configuration Using a New Minimum Infinity-Norm Solution," Aerospace Science and Technology, Vol. 39, 2014, pp. 109-119. https://doi.org/10.1016/j.ast.2014.09.002
- Bialke, B., "High Fidelity Mathematical Modeling of Reaction Wheel Performance," Annual Rocky Mountain Guidance and Control Conference, 1998, pp. 483-496, AAS 98-063.
- Carrara, V., and Kuga, H. K., "Estimating Parameters in Reaction Wheels for Attitude Control," Mathematical Problems in Engineering, Vol. 2013, 2013, pp. 1-9.
- Cao, X., and Wu, B., "Indirect Adaptive Control for Attitude Tracking of Spacecraft With Unknown Reaction Wheel Friction," Aerospace Science and Technology, Vol. 47, 2015, pp. 493-500. https://doi.org/10.1016/j.ast.2015.10.017
- Son, J.-W., and Park, Y.-W., "Relation between Reaction Wheel Speed Detection Method and Drag Compensation," Proceeding of The Korean Society for Aeronautical and Space Sciences Fall Conference, November 2017, pp. 645-646.