Abstract
The Lagrange brackets, \(\left [{c_j},{c_k}\right ]\), must be evaluated in terms of the orbital elements and a particular coordinate frame so that
may be solved for the \({{\dot {c}}_{k}}\) (i.e., to find the differential equations). (See Eq. 3.41.)
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Longuski, J.M., Hoots, F.R., Pollock IV, G.E. (2022). Evaluation of the Lagrange Brackets. In: Introduction to Orbital Perturbations. Space Technology Library, vol 40. Springer, Cham. https://doi.org/10.1007/978-3-030-89758-1_4
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