Linearized dynamics of rotating aerospace vehicles with internal angular momenta

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049 ⊔ ⊔ ‡aMAIN
086 0 ⊔ ‡aD 301.45/26:61-63
088 ⊔ ⊔ ‡aAD 268628
088 ⊔ ⊔ ‡aASD TN 61-63
100 1 ⊔ ‡aMcRuer, Duane T., ‡eauthor.
245 1 0 ‡aLinearized dynamics of rotating aerospace vehicles with internal angular momenta / ‡cDuane T. McRuer, Julian Wolkovitch.
264 ⊔ 1 ‡aWright-Patterson Air Force Base, Ohio : ‡bAeronautical Systems Division, Air Force Systems Command, United States Air Force, ‡c1961.
300 ⊔ ⊔ ‡aviii, 22 pages : ‡billustrations, figures, tables ; ‡c28 cm
336 ⊔ ⊔ ‡atext ‡btxt ‡2rdacontent
337 ⊔ ⊔ ‡aunmediated ‡bn ‡2rdamedia
338 ⊔ ⊔ ‡avolume ‡bnc ‡2rdacarrier
490 0 ⊔ ‡aAeronautical Systems Division (U.S.). Technical Note ; ‡vASD TN 61-63
500 ⊔ ⊔ ‡a"The research was performed by Systems Technology, Inc."
500 ⊔ ⊔ ‡aAD0268628 (from http://www.dtic.mil).
500 ⊔ ⊔ ‡a"July 1961."
504 ⊔ ⊔ ‡aIncludes bibliographical references (page 22).
520 ⊔ ⊔ ‡aThe coupling of longitudinal and lateral motions arising from the gyroscopic effects of internal rotating parts, and from inertial cross-coupling is considered. Equations of motion are reduced to a four-degrees-of-freedom set by neglecting perturbations in the rolling velocity and forward speed as measured in a special axis system. A quartic characteristic equation results which contains the effects of steady-state lateral angular and pitching velocities. This quartic can be regarded as the characteristic equation of a hypothetical closed-loop system and the roots, critical internal angular velocity, etc., can be obtained by standard graphical servo techniques. Examples of the application of these techniques are presented to show that this approach indicates the salient features of the coupled motions, predicts any stability deficiencies that may exist, and enables the effects of parameter changes to be analyzed swiftly.
536 ⊔ ⊔ ‡aAir Force Contract No. ‡bAF 33(616)-5961, Project No. 8219, Task No. 82162.
538 ⊔ ⊔ ‡aMode of access: Internet.
650 ⊔ 0 ‡aMathematical analysis.
650 ⊔ 0 ‡aRotational motion (Rigid dynamics)
650 ⊔ 0 ‡aGyroscopic instruments.
650 ⊔ 0 ‡aFlight control.
650 ⊔ 0 ‡aAirframes.
700 1 ⊔ ‡aWolkovitch, Julian, ‡eauthor.
710 1 ⊔ ‡aUnited States. ‡bAir Force. ‡bSystems Command. ‡bAeronautical Systems Division. ‡esponsor.
710 1 ⊔ ‡aUnited States. ‡bAir Force. ‡bSystems Command, ‡eissuing agency
710 2 ⊔ ‡aSystems Technology, Inc., ‡esponsor.
710 2 ⊔ ‡aSystems Technology, Inc.
710 1 ⊔ ‡aUnited States. ‡bAir Force. ‡bSystems Command. ‡bAeronautical Systems Division.
730 0 ⊔ ‡aTechnical Report Archive & Image Library (TRAIL)
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DAT 1 ⊔ ‡a20230928062550.0 ‡b2024-06-26T17:54:41Z
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