On the formulation of equations of rotational motion for an N-body spacecraft
By: prepared for Space and Missile Systems Organization, Air Force Systems Command.
Contributors: Aerospace Corporation; Space and Missile Systems Organization (U.S.)
Publisher: Aerospace Corporation
Published: 1969
Place of publication: El Segundo, Calif
Number of pages: 53
Subjects: Angular momentum; Equations of motion; Rotating bodies; Spacecraft
Notes: Bibliographical refrences: p.53.