Abstract
a = semimajor axis E = eccentric anomaly e = eccentricity F = thrust acceleration FR;W;S = radial, normal, and circumferential thrust acceleration i = inclination M = mean anomaly r = radial unit vector ŵ = normal unit vector α k = cosine coefficient, Fourier series of thrust acceleration β k = sine coefficient, Fourier series of thrust acceleration ΔV = velocity increment λ = angle of thrust acceleration Ω = longitude of the ascending node ω = argument of periapsis
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