Beyers, ME2008-04-142008-04-141975Beyers, ME. 1975. Technique for smoothing free-flight oscillation data. Journal of Spacecraft and Rockets, vol 12(5), pp 318-3190022-4650http://hdl.handle.net/10204/2230Copyright: 1975 American Institute of Aeronautics and AstronauticsA technique based on superposition of tricyclic solutions has been proposed for smoothing free-flight angular motion. When incorporated into a conventional tricyclic data reduction program, the method is convenient to use and does not require a separate smooting routine. Tricyclic motion components determined in the smoothing process can be related to effects of individual nonlinearities on the motion.enOscillation dataFree-flight motionArticleBeyers, M. (1975). Technique for smoothing free-flight oscillation data. http://hdl.handle.net/10204/2230Beyers, ME "Technique for smoothing free-flight oscillation data." (1975) http://hdl.handle.net/10204/2230Beyers M. Technique for smoothing free-flight oscillation data. 1975; http://hdl.handle.net/10204/2230.TY - Article AU - Beyers, ME AB - A technique based on superposition of tricyclic solutions has been proposed for smoothing free-flight angular motion. When incorporated into a conventional tricyclic data reduction program, the method is convenient to use and does not require a separate smooting routine. Tricyclic motion components determined in the smoothing process can be related to effects of individual nonlinearities on the motion. DA - 1975 DB - ResearchSpace DP - CSIR KW - Oscillation data KW - Free-flight motion LK - https://researchspace.csir.co.za PY - 1975 SM - 0022-4650 T1 - Technique for smoothing free-flight oscillation data TI - Technique for smoothing free-flight oscillation data UR - http://hdl.handle.net/10204/2230 ER -