CALCULATED RESONANT PREQUENCIES OF THE FOUR-LEGGED SUPPORT STRUCTURE FOR THE SECONDARY MIRROR (QUADRUPOD) Calculated Measured Mode Frequency Frequency* Nature of Vibration ____________________________________________________________________________ 1 17.2 cps 16.4 cps Torsional (about optical axis) 2 33.5 (34 Legs flexing (fundamental) 3 33.5 34 Legs flexing (different phase) 4 35.7 (34) Legs flexing (symmetrical) 5 48.7 48.6 (to 51) Torsional (1. overtone) 6 59.8 66 Top moves in x direction 7 59.8 66 Top moves in y direction 8 72.5 73.6 Squatting in z direction? 9 76.2 93 Top moves in x direction 10 76.2 93 Top moves in y direction 11 81.9 86.2 Squatting in z direction? 12 96.8 Legs flexing 13 102.8 Legs flexing, top fixed 14 102.8 Diffn. phasing of mode 13 15 108.5 Torsional, (2. overtone) 16 185.3 Legs flexing, top fixed 17 186.7 Top displaced 18 186.7 Diffn phase of mode 18 19 194.3 Top displaced in x 20 194.3 Top displaced in y ____________________________________________________________________________ For these calculations, the Z axis is along the optical axis, and the X and Y axes are orthogonal to it, along lines through opposite sets of feet of the quadrupod. Measurements (*) of the natural frequencies of this structure in the actual telescope by a Modal and Control Dynamics Team at Marshall Space Flight Center founnd the first two torsional modes at 16.4 cps (vs 17.2 in the calculation) and 48.6 cps (vs 48.7). We have identified the other modes tentatively by sorting through resonances measured for different axes at a point on the side of the top cylinder and at a point on one of the struts. All these modes result from various ways the four legs bend, as you can see from the plots. The swaying modes, in which opposing legs shorten and lengthen out of phase, namely modes 6&7 and 9&10, are probably shifted to higher frequency because we tensioned the guy wires more than in the calculations.