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Evaluation of the Lagrange Brackets

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Introduction to Orbital Perturbations

Part of the book series: Space Technology Library ((SPTL,volume 40))

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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

$$\displaystyle \sum \limits _{k=1}^{6}{\left [ {{c}_{j}},{{c}_{k}} \right ]}{{\dot {c}}_{k}}=\mathbf {F}\cdot \frac {\partial \mathbf {r}}{\partial {{c}_{j}}}, \hspace {0.5in} j=1,2,\dots ,6 $$

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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