On the Application of Perturbation Technique to the Study of Missile Flight with Special Reference to Internal Mass Flow, Thrust Malalignments, and the Effect of Gravity
On the Application of Perturbation Technique to the Study of Missile Flight with Special Reference to Internal Mass Flow, Thrust Malalignments, and the Effect of Gravity
- New search for: M. A. Ranta
- New search for: M. A. Ranta
For the stability of missiles in rectilinear flight with an arbitrary inclination, special attention is paid to some secondary factors usually neglected. They are: the diminishing mass of the missile; the mass flow inside the missile; the imperfections in the resulting thrust called malalignments; and the effect of gravity. The treatment is based on the perturbation method applied to Euler's equations of motion, and on the Laplace transforms and the Wiener-Hopf technique. The stability criterion is derived from the approximate solution for small values of time. A numerical example is given. (Author)
Document information
On the Application of Perturbation Technique to the Study of Missile Flight with Special Reference to Internal Mass Flow, Thrust Malalignments, and the Effect of Gravity
1969
43 pages
Report
No indication
English
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