Now consider one method of selecting feedback gains which will make the linearized system behave as though it were time-invariant. First make the definition (6-16) where K1,1(t) corresponds to feedback of the joint positions and K1,2(t) corresponds to feedback of the joint velocities. Using (6-11) through (6-13) it is possible to write the linearized system matrix as F*(t) -G L -BH (6-17) INxN F2(t) - d-l1 (6**)Ki,2(t) 0 0 -JO )K2(t) A We desire a feedback law which will make the right-hand side of (6-17) take the following form 0 Mi -B INx M2 0 (6-18) where M, c RNxN, M2 E RNxN, and M3 e RNxrN are constant matrices (note that A e RrNxrN). It can be shown that the eigenvalues of (6-18) can be assigned arbitrarily by proper choice of M1, M2 and M3. This is, in 0 Fl1(t) - J-l( *)Kl1,l(t) -B Klmt := [Kl,l(t), K1,2(t)]