Path-length control for a reflector antenna using piezoelectric actuators and a focus adjustment mechanism

Author:

TANAKA Hiroaki1

Affiliation:

1. Department of Aerospace Engineering, National defense academy of Japan

Publisher

Japan Society of Mechanical Engineers

Reference18 articles.

1. Belvin, K., Edighoffer, H. H. and Herstrom, C. L., Quasistatic shape adjustment of a 15-m-diameter space antenna, Journal of Spacecraft and Rockets, Vol.26 (1989), pp.129-136.

2. Bradford, S.C., Peterson, L.D., Ohara, C.M., Fang, S., Agnes, G.S., Hoffman, S.M. and Wilkie, W.K., Piezocomposite actuator arrays for correcting and controlling wavefront error in reflectors, 53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, AIAA 2012-1828 (2012), pp.1-15.

3. Datashvili, L., Baier, H., Wei, B., Hoffman, J., Wehrle, E., Schreider, L., Mangenot, C., Prowald, J.S., Scolamiero, L. and Angevain, J.C., Mechanical investigations of in-space-reconfigurable reflecting surfaces, 32nd ESA Antenna Workshop on Antennas for Space Applications (2010).

4. Haftka, R.T., Limits on static shape control for space structures, AIAA Journal, Vol. 29, No. 11 (1991), pp. 1945-1950.

5. Hanayama, E. and Takano, T., Investigation of radiation characteristics of large deployable antennas using a model antenna, The transactions of the Institute of Electronics, Information and Communication Engineers. B-II, Vol.J75-B-2, No.6 (1992), pp. 285-292 (in Japanese).

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