AIAA Guidance, Navigation, and Control Conference 2011
DOI: 10.2514/6.2011-6730
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Solar Dynamics Observatory On-orbit Jitter Testing, Analysis, and Mitigation Plans

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Cited by 9 publications
(5 citation statements)
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“…Because the entire machine is tested, two methods can be used to simulate the micro-vibration environment: the first is to use real disturbance equipment such as a flight reaction wheel, and the second is to use a simulator. Liu et al (2007) used a flight reaction wheel to generate the required disturbance and connected it to a structural verification unit to measure the degree of disturbance produced by the flight reaction wheel. However, disturbance generation using the flight reaction wheel increases the experimental costs greatly and requires a high level of research funding.…”
Section: Introductionmentioning
confidence: 99%
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“…Because the entire machine is tested, two methods can be used to simulate the micro-vibration environment: the first is to use real disturbance equipment such as a flight reaction wheel, and the second is to use a simulator. Liu et al (2007) used a flight reaction wheel to generate the required disturbance and connected it to a structural verification unit to measure the degree of disturbance produced by the flight reaction wheel. However, disturbance generation using the flight reaction wheel increases the experimental costs greatly and requires a high level of research funding.…”
Section: Introductionmentioning
confidence: 99%
“…Liu et al (2007) used a flight reaction wheel to generate the required disturbance and connected it to a structural verification unit to measure the degree of disturbance produced by the flight reaction wheel. However, disturbance generation using the flight reaction wheel increases the experimental costs greatly and requires a high level of research funding.…”
Section: Introductionmentioning
confidence: 99%
“…However, the MHD ARS does not possess the capability of measurement at low frequency (<1 Hz), especially the constant inertial angular rate [ 12 ], which is essential for precision LOS pointing and wide-bandwidth LOS jitter suppression [ 13 , 14 ]. Martin et al [ 15 ] investigated whether the differential of MHD ARS could be used to measure head angular acceleration in impact testing.…”
Section: Introductionmentioning
confidence: 99%
“…While for MEMS gyroscopes the reliability and shock resistance issues [ 9 ] are still open and micro integrated optic gyros have serious critical aspect in reducing the influence of noise sources especially in a wide bandwidth [ 10 ], in fact, there are some applications where very small angles in vibration environments need to be measured and controlled precisely. On-orbit jitter measurement in line-of-sight (LOS) stabilization system [ 11 ], space borne Earth observation [ 12 ] and Solar Dynamic Observatory [ 13 ] are examples of such environments where ultralow measurement noise (<1 μrad/s(rms)) [ 14 ] with wide bandwidth [ 15 ] is demanded. The magnetohydrodynamic (MHD) angular rate sensor (ARS) has no mechanical saturation allowing rapid recovery from large angle slews and low measurement noise levels without additional increased complexity in ultra-wideband.…”
Section: Introductionmentioning
confidence: 99%