E. I. KHARLAMOVA, P. V. KHARLAMOV
Unknown
Submitted 1969-01-01 | RussiaRxiv: ru-196901.76724 | Translated from Russian

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E. I. KHARLAMOVA, P. V. KHARLAMOV

A NEW CASE OF INTEGRABILITY OF THE EQUATIONS OF MOTION OF A HEAVY RIGID BODY HAVING A FIXED POINT

(Presented by Academician P. Ya. Kochina on 28 II 1969)

The Euler–Poisson equations for the problem of the motion of a heavy rigid body in the case when the center of gravity lies on the first principal axis, and the gyrostatic moment is orthogonal to the third axis, have the form

\[ \begin{aligned} A\,dp/dt &= (B-C)qr+\lambda_2 r,\\ B\,dq/dt &= (C-A)rp-\lambda_1 r+\Gamma v_1,\\ C\,dr/dt &= (A-B)pq+\lambda_1 q-\lambda_2 p+\Gamma v_2,\\ dv_1/dt &= rv_2-qv_3,\quad dv_2/dt = pv_3-pv_1,\quad dv_3/dt = qv_1-pv_2. \end{aligned} \tag{1} \]

Here \(v_1, v_2, v_3\) are the components of the unit vector in the direction of the force of gravity; \(\Gamma\) is the product of the weight of the body and the distance from the fixed point to the center of gravity; \(\lambda_1, \lambda_2, 0\) are the gyrostatic moment; the remaining notation is standard.

The known integrals of these equations are:

\[ Ap^2+Bq^2+Cr^2-2\Gamma v_1=2E, \]

\[ (Ap+\lambda_1)v_1+(Bq+\lambda_2)v_2+Crv_3=k/\Gamma, \]

\[ v_1^2+v_2^2+v_3^2=1. \]

Let us subject the moments of inertia to the condition

\[ A=18C(B-C)/(10B-9C), \]

and, instead of \(\lambda_1,\lambda_2\), introduce the parameters \(u\) and \(\varepsilon\), putting

\[ \lambda_1=\frac{u}{9}\, \frac{25B^2-54BC+27C^2}{B^2C(10B-9C)}\,n\cos\varepsilon, \quad \lambda_2=-\frac{u}{3}\, \frac{(B-C)^2}{B^2C^2}\,n\sin\varepsilon. \]

Equations (1) then have, in this case, a solution in which the principal variables \(p,q,r,v_1,v_2,v_3\), expressed as functions of the new variable \(\sigma\), are as follows:

\[ p=-u\,\frac{B-C}{ABC} \left(\frac{1}{B}\frac{5B-3C}{10B-9C}n\cos\varepsilon+2\cos\sigma\right), \]

\[ q=\frac{u}{3BC} \left(\frac{B-C}{BC}n\sin\varepsilon-2\sin\sigma\right), \]

\[ r=\frac{u}{C} \left(r_0+r_1\cos\sigma+r'_1\sin\sigma+r_2\cos2\sigma+r_3\cos3\sigma+r'_3\sin3\sigma\right)^{1/2}, \]

\[ v_1=-\frac{u^2}{\Gamma}\frac{2B-3C}{36BC^2} \left(\chi_0+\chi_1\cos\sigma+\chi'_1\sin\sigma+\chi_2\cos2\sigma+\chi_3\cos3\sigma+\chi'_3\sin3\sigma\right), \]

\[ v_2=-\frac{u^2}{\Gamma}\frac{2B-3C}{36BC^2} \left(\chi_0+\chi_1\cos\sigma+\chi'_1\sin\sigma+\chi'_2\sin2\sigma+\chi_3\cos3\sigma+\chi'_3\sin3\sigma\right), \]

\[ v_3=\frac{u}{\Gamma}\frac{1}{18C}\left[-\frac{B-C}{B^2C}h\cos\varepsilon+ \frac{6(2B-3C)}{BC}\cos\sigma\right] \left(r_0+r_1\cos\sigma+r'_1\sin\sigma+ \right. \]
\[ \left. +r_2\cos2\sigma+r_3\cos3\sigma+r'_3\sin3\sigma\right)^{1/2}, \]

where

\[ r_0=2E_*-\frac{2B-3C}{27B^2C^3}(16B^2+13BC-18C^2)+ \]
\[ +\frac{1}{162B^3C^2}\left[18\frac{(B-C)^2}{C} -\frac{(5B-3C)(35B-33C)}{10B-9C}\right]n^2\cos^2\varepsilon, \]

\[ r_1=-\frac{1}{36}\frac{(B-C)(50B-27C)}{B^3C^2}\,n\cos\varepsilon, \]

\[ r'_1=\frac{1}{36}\frac{(B-C)(10B+9C)}{B^3C^2}\,n\sin\varepsilon, \]

\[ r_2=-\frac{1}{9}\frac{(2B-3C)(11B-6C)}{B^2C^2},\qquad n^2=\frac{4}{3}\frac{(2B-3C)(4B-3C)B^2}{(B-C)^2}, \]

\[ r_3=-\frac{1}{12}\frac{(B-C)(2B-3C)}{B^3C^2}\,n\cos\varepsilon, \]

\[ r'_3=-\frac{1}{12}\frac{(B-C)(2B-3C)}{B^3C^2}\,n\sin\varepsilon, \]

\[ \varkappa_0=\frac{3}{2}\frac{10B-9C}{BC} -\frac{(B-3C)(5B-3C)}{9B^3C(2B-3C)}\,n^2\cos^2\varepsilon, \]

\[ \varkappa_1=\frac{1}{3B^2C}\left(\frac{5B+3C}{2} +\frac{10B^2-15BC+9C^2}{2B-3C}\right)n\cos\varepsilon, \qquad \varkappa'_1=\frac{3}{2}\frac{B-C}{B^2C}\,n\sin\varepsilon, \]

\[ \varkappa_2=\frac{6(2B-C)}{BC},\qquad \varkappa_3=\frac{3(B-C)}{2B^2C}\,n\cos\varepsilon,\qquad \varkappa'_3=\frac{3(B-C)}{2B^2C}\,n\sin\varepsilon, \]

\[ \chi_0=-\frac{2(B-C)(B-3C)}{B^3C(2B-3C)}\,n^2\cos\varepsilon\sin\varepsilon,\qquad \chi_1=-\frac{9}{2}\frac{B-C}{B^2C}\,n\sin\varepsilon, \]

\[ \chi'_1=\frac{1}{3B^2C}\left(-\frac{5B+3C}{2} +\frac{10B^2-15BC+9C^2}{2B-3C}\right)n\cos\varepsilon, \qquad \chi'_2=\frac{8}{C}, \]

\[ \chi_3=-\frac{3(B-C)}{2B^2C}\,n\sin\varepsilon,\qquad \chi'_3=\frac{3(B-C)}{2B^2C}\,n\cos\varepsilon, \]

\[ E_*=\frac{4}{27}\frac{(B-2C)(4B-3C)}{BC^3} +\frac{1}{5184B^2}\left[ 3\frac{(B-3C)^2}{B^2C^2}\frac{10B-7C}{2B-3C} +9\frac{5B-3C}{B^2C^2}\times \right. \]
\[ \left. \times\frac{6B-7C}{10B-9C} -2(34B-51C)(5B-3C)\frac{B-3C}{2B-3C} -36\frac{(B-C)^2(8B-9C)}{B^2C^3} \right]n^2\cos^2\varepsilon \]

The dependence between \(\sigma\) and \(t\) is established by inverting the integral

\[ t-t_0=\frac{3(B-C)}{uB}\int_0^\sigma \left(r_0+r_1\cos\sigma+r'_1\sin\sigma+r_2\cos2\sigma+ \right. \]
\[ \left. +r_3\cos3\sigma+r'_3\sin3\sigma\right)^{-1/2}\,d\sigma \]

The parameters \(B,C,\Gamma,\varepsilon\) in this solution are independent.

Donetsk Computing Center
of the Academy of Sciences of the Ukrainian SSR

Received
21 II 1969

Submission history

E. I. KHARLAMOVA, P. V. KHARLAMOV