This paper studies the attitude dynamics of variable mass systems that have axisymmetric mass distribution and that are subjected to continuous mass variation while in motion. The equations of rotational motion for such systems are solved analytically under the assumption of zero external torque. It is found that such systems can spin up or spin down in free motion, and that the transverse angular velocity magnitude can increase or decrease with time. The analytical conditions for growth or decay of spin rate and lateral angular speed are presented, and these conditions are related to practical design criteria for rocket-type systems.
Issue Section:
Technical Papers
1.
Bernoulli, D., 1738, Hydrodynamica, Argentorati.
2.
Eke
F. O.
Wang
S. M.
1994
, “Equations of Motion of Two-Phase Variable Mass Systems with Solid Base
,” ASME JOURNAL OF APPLIED MECHANICS
, Vol. 61
, pp. 855
–860
.3.
Eke, F. O., and Wang, S. M., 1995, “Attitude Behavior of A Variable Mass Cylinder,” ASME JOURNAL OF APPLIED MECHANICS, to appear.
4.
Ellis
J. W.
McArthur
C. W.
1959
, “Applicability of Euler’s Dynamical Equations to Rocket Motion
,” ARS Journal
, Vol. 29
, No. 11
, pp. 867
–864
.5.
Meirovitch
L.
1970
, “General Motion of a Variable Mass Flexible Rocket with Internal Flow
,” Journal of Spacecraft and Rockets
, Vol. 7
, No. 2
, pp. 186
–195
.6.
Rosser, J. B., Newton, R. R., and Cross, G. L., 1947, Mathematical Theory of Rocket Flight, McGraw-Hill, New York.
7.
Thomson, W. T., 1963, Introduction to Space Dynamics, John Wiley and Sons, New York.
8.
Thomson
W. T.
Reiter
G. S.
1965
, “Jet Damping of a Solid Rocket: Theory and Flight Results
,” AIAA Journal
, Vol. 3
, No. 3
, pp. 413
–417
.9.
Wang, S. M., 1993, “Attitude Dynamics of Variable Mass Systems,” Ph.D. Dissertation, University of California, Davis, CA.
10.
Warner
G. G.
Snyder
V. W.
1968
, “A Re-Evaluation of Jet Damping
,” J. Spacecraft
, Vol. 5
, No. 3
, pp. 364
–366
.
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