2007
DOI: 10.2514/1.22984
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Primer Vector Theory Applied to Global Low-Thrust Trade Studies

Abstract: The low-thrust spacecraft trajectory problem can be reduced to only a few parameters using calculus of variations and the well-known primer vector theory. This low dimensionality combined with the extraordinary speed of modern computers allows for rapid exploration of the parameter space and invites opportunities for global optimization. Accordingly, a general low-thrust trade analysis tool is developed based on a global search for local indirect method solutions. An efficient propagator is implemented with an… Show more

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Cited by 143 publications
(79 citation statements)
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“…To improve accuracy in computing the Jacobian of the shooting function, it is obtained by analytic derivatives [21]. The procedure for obtaining analytical derivatives requires the use of the state transition matrix (STM) of Eq.…”
Section: Analytic Jacobians Matrixmentioning
confidence: 99%
See 1 more Smart Citation
“…To improve accuracy in computing the Jacobian of the shooting function, it is obtained by analytic derivatives [21]. The procedure for obtaining analytical derivatives requires the use of the state transition matrix (STM) of Eq.…”
Section: Analytic Jacobians Matrixmentioning
confidence: 99%
“…(36), valid only when 蔚 > 0. For the fuel optimal problem (蔚 = 0), a chain rule should be applied to string together a sequence of partial derivatives with "bangbang" switching point between them [21].…”
Section: Analytic Jacobians Matrixmentioning
confidence: 99%
“…Studies on the indirect methods are mainly focused on efficient numerical solving techniques. Using primary vector theory, Russel [29] investigated indirect solving methods for fuel optimal problem. Bertrand et al [30] proposed the homotopy idea for indirect low thrust optimization, they first optimized performance indicators that are easy to solve and then used the stepwise iterative method for fuel optimization.…”
Section: Low Thrust Trajectory Optimizationmentioning
confidence: 99%
“…FIRE is particularly suited for problems that favor higher speeds and smooth derivatives, such as trajectory optimization (Russell 2007(Russell , 2004Hull 1979;Sauer 1989), orbit determination (Campbell and Speckman 2004;Russell and Lara 2007;Koon et al 1999;Lo et al 2004) and Monte Carlo sensitivity analysis (Desai and Cheatwood 1999;Aiello 2005). The new system generally favors speed in sacrifice of relatively more memory.…”
mentioning
confidence: 98%