Determination of the efficacy of using accelerometers as sensors for third generation satellites
By: Peter Robert Wilhelm Dietz.
Contributors: UTIAS
Series: UTIAS technical note -- no.262
Publisher: Institute for Aerospace Studies
Published: 1986
Place of publication: [Downsview, Ont.]
Number of pages: 84
Subjects: Acceleration feedback; Attitude control; Flexible spacecraft
Notes: Bibliographical references: p.11.