Ensuring Control Processes Quality in Relay System Without Speed Sensor

Simonyants, R.P.

doi:10.7463/1014.0729606

S&E BMSTU

2014

DOI: 10.7463/1014.0729606

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Ensuring Control Processes Quality in Relay System Without Speed Sensor

R.P. Simonyants¹

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Cited by 2 publications

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Investigating the “inverted attitude” problem in a spacecraft stabilisation system featuring non-linear sensors

Simonyants

Тарасов

2020

EJSI

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The paper shows that gravitational torque may cause an emergency “inverted attitude” mode in a relay spacecraft stabilisation system due to the fact that a field-of-view limit type sensor may be non-linear. We performed structural partitioning of the phase cylinder into regions with various trajectory types for the case of a simplified planar motion model. We demonstrate the synthesis routine for finding the boundaries separating the region marking the system transitioning into the regular attitude mode from the region signifying it entering the emergency mode. We derived analytical conditions under which emergency modes arise, which can serve as the basis for synthesising algorithms to prevent these modes from occurring.

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Investigating the “inverted attitude” problem in a spacecraft stabilisation system featuring non-linear sensors

Simonyants

Тарасов

2020

EJSI

View full text Add to dashboard Cite

show abstract

Defining the Spacecraft Angular Position in the Orbital Stabilization Mode from the Angular Rate Sensor Measurements

Oleynik¹,

Ryabchenko²

2014

S&E BMSTU

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Ensuring Control Processes Quality in Relay System Without Speed Sensor

Cited by 2 publications

References 5 publications

Investigating the “inverted attitude” problem in a spacecraft stabilisation system featuring non-linear sensors

Investigating the “inverted attitude” problem in a spacecraft stabilisation system featuring non-linear sensors

Defining the Spacecraft Angular Position in the Orbital Stabilization Mode from the Angular Rate Sensor Measurements

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