Several of us presented at the recent Roman Coronagraph Instrument Information Sessions, held virtually on October 26th and 28th. Slides and recordings of all talks are available here.
Also, check out the results of the Coronagraph Science Investigation Team at romancgi.sioslab.com
“Higher-Order Unscented Estimator” by Zvonimir Stojanovski and Dmitry Savransky has been published in the Journal of Guidance, Control and Dynamics. It is available here (open access). This paper introduces HOUSE, a new extension of the unscented Kalman (UKF) filter with asymmetric sample points and weights chosen to match third- and fourth-order moments in addition to the mean and covariance. Compared with the conventional UKF and conjugate unscented transform (CUT) filters, HOUSE is shown to be more robust to outliers in the process and measurement noise.
Our latest paper, Keithly & Savransky, “The Solar System as an Exosystem: Planet Confusion“, is now published in the Astrophysical Journal Letters. This work explores the idea of what we can learn about observing other planetary systems by thinking about external observers studying our own solar system, and the issues they might run into. The Cornell Chronicle has a great story summarizing the research (also carried at Phys.org).
Our newest paper: Keithly, Savransky, and Spohn, “Integration Time Adjusted Completeness” is now available as open access in the Journal of Astronomical Telescopes, Instruments, and Systems. This paper updates the concept of completeness—the probability of detecting an exoplanet from some population with a specific instrument—to take into account the required integration time, showing that previous calculations of completeness have been overestimating these probabilities.
I’ve been teaching the theory of nutation dampers for years, and have finally gotten around to creating a good visualization of one. Nutation dampers are really neat devices for rejecting disturbances on spin-stabilized spacecraft. Essentially, a damper is any mechanical device with energy dissipation that is excited by spin about a transverse spacecraft axis. The dissipation mechanism causes the non-symmetry axis spin to diminish over time, and the spacecraft returns to pure symmetry axis spin. Physical implementations can range from spring-mass-damper systems to wheels mounted on a transverse spacecraft axis whose spin results in any sort of viscous damping. Here’s an animation of the latter sort. The spacecraft (blue cylinder) is a major-axis spinner, and experiences an angular impulse after five revolutions, which spins up the nutation damper (red wheel). Over time, the spacecraft settles back into pure symmetry axis spin.
The plots show the time histories of the components of spacecraft angular velocity (\omega_2 is the spin about the symmetry axis) as well as the damper’s spin rate (\Omega).
I recently had the opportunity to do a guest lecture on astronomy space missions. See below for some fun facts about Hubble and other space telescopes.