In the video linked in this answer the spacecraft is said to be "gyroscopically balanced" (at about 00:20).
I'm going to ask about the terminology associated with the phrase "gyroscopic stabilization" - attitude control of a spacecraft which involves the use of gyroscopes.
Here is what I believe is true: A gyroscope is traditionally a rotating wheel in a mount that contains additional degrees of freedom. The term "scope" suggests some kind of measurement, and while a gyroscope can be a rotating wheel, it can also be a ring of optical fiber (or other waveguide) or a micro-fabricated Micro-electromechanical systems (MEMS) chip.
So if a spacecraft uses gyroscopes that do not contain rotating wheels, and it uses thrusters or magnetotorquers or solar reflectors for torque, can we still correctly say that it is gyroscopically stablized without the use of any rotating parts?