MOTIONVARIABLES' Q{2}''
CONSTANTS L,M,G
NEWTONIAN N
POINT PN
V_PN_N> = 0>
THETA1 = ATAN(Q2/Q1)
FRAMES A
SIMPROT(N, A, 3, THETA1)
PARTICLES P
P_PN_P> = Q1*N1>+Q2*N2>
MASS P=M
V_P_N>=DT(P_P_PN>, N)
F_V = DOT(EXPRESS(V_P_N>,A), A1>)
GRAVITY(G*N1>)
DEPENDENT[1] = F_V
CONSTRAIN(DEPENDENT[Q1'])
ZERO=FR()+FRSTAR()
F_C = MAG(P_P_PN>)-L
CONFIG[1]=F_C
ZERO[2]=CONFIG[1]
