Author:
Jonckheere Edmond A.,Silverman Leonard M.
Reference41 articles.
1. W. B. Gevarter, “Basic relations for the control of flexible vehicles,” AIAA 7th Aerospace Sciences Meeting, New York City, New York, January 20–22, 1969, AIAA Paper No. 69-115.
2. G. Porcelli, “Attitude control of flexible space vehicles,” AIAA Journal, vol. 10, pp. 807–812, June 1972.
3. V. J. Modi, “Attitude dynamics of satellites with flexible appendages — a brief review,” J. Spacecraft, vol. 11, pp. 743–751, November 1974.
4. M. Healey et al., “Design of a digital-stability augmentation and control system with gust alleviations and modal suppression,” Proc. IEE, vol. 112, pp. 437–440, April 1975.
5. J. E. Cochran and D.E. Christensen, “Free-flight rocket attitude motion due to transverse vibration,” J. Spacecraft, vol. 17, pp. 425–431, Sept.-Oct. 1980.
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