Author
J. C. Nicklas
Bio: J. C. Nicklas is an academic researcher from Jet Propulsion Laboratory. The author has contributed to research in topics: Attitude control & Control system. The author has an hindex of 1, co-authored 1 publications receiving 21 citations.
Topics: Attitude control, Control system
Papers
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01 Jan 1963
TL;DR: In this paper, a parametric analysis of the magnitudes and directions of solar pressure torques is performed to optimize the attitude control system of a spacecraft attitude by parametric optimization.
Abstract: Spacecraft attitude control system optimization by parametric analysis of the magnitudes and directions of solar pressure torques
30 citations
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TL;DR: In this paper, the kinematic equations of motion are used as a system model with the gyro signals considered as known-forcing functions, and the Kalman-Bucy filter corresponding to this improved gyro model produces significantly smaller error variances in yaw angle than the orbital gyrocompass, largely through estimation of the yaw-gyro drift.
24 citations
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15 citations
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TL;DR: A method for finding the loci of points in state space at which the steering functions should be switched to the opposite direction is illustrated and a constant which describes the degree of asymmetry is described.
14 citations