3rd Tethers in Space/ Toward Flight International Conference 1989
DOI: 10.2514/6.1989-1563
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Tethered Dynamics Explorer and Tethered Atmospheric Probe - A low-cost, low-risk tethered satellite program

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Cited by 3 publications
(6 citation statements)
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“…A mass of 22 g was placed on the end of the tether to produce a static tension in the tether, which is slightly larger than the static tension the actual system will experience when fully deployed. 2 In such a configuration, the equations of motion governing the pendu- lum system are analogous to those of the system model used by Rupp 4 and Baker et al, 5 if air damping is ignored. Using a Lagrangian formulation, the equations are…”
Section: System Equationsmentioning
confidence: 97%
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“…A mass of 22 g was placed on the end of the tether to produce a static tension in the tether, which is slightly larger than the static tension the actual system will experience when fully deployed. 2 In such a configuration, the equations of motion governing the pendu- lum system are analogous to those of the system model used by Rupp 4 and Baker et al, 5 if air damping is ignored. Using a Lagrangian formulation, the equations are…”
Section: System Equationsmentioning
confidence: 97%
“…2 The classical family of Bode magnitude and phase curves depicted in any standard text on vibrations, dynarnic systems, or control theory illustrates this dependency. It is seen that the slope of the phase curve at the point (GJ W , -90 deg) varies over a wide range from the critically damped ({"= 1) to the undamped (f=0).…”
Section: Second-order Systemmentioning
confidence: 98%
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“…Several ideas to support and accelerate the GNC development using demonstrators have been conceived in the past, for example NASA's Morpheus lander [1,2] or the HOMER demonstrator of Airbus Defense and Space [3,4]. In these and other developments of space systems, a wide variety of tethered experimental setups has been created [1,2,[5][6][7][8].…”
Section: Introductionmentioning
confidence: 99%