2009
DOI: 10.1007/s10589-009-9291-0
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Direct trajectory optimization and costate estimation of finite-horizon and infinite-horizon optimal control problems using a Radau pseudospectral method

Abstract: A method is presented for direct trajectory optimization and costate estimation using global collocation at Legendre-Gauss-Radau (LGR) points. The method is formulated first by casting the dynamics in integral form and computing the integral from the initial point to the interior LGR points and the terminal point. The resulting integration matrix is nonsingular and thus can be inverted so as to express the dynamics in inverse integral form. Then, by appropriate choice of the approximation for the state, a pseu… Show more

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Cited by 319 publications
(285 citation statements)
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References 23 publications
(11 reference statements)
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“…[18][19][20] In the Radau pseudospectral method, the state and its time derivative are approximated, respectively, in each mesh interval S k , (k = 1, . .…”
Section: Radau Pseudospectral Methods For Problem Mmentioning
confidence: 99%
See 2 more Smart Citations
“…[18][19][20] In the Radau pseudospectral method, the state and its time derivative are approximated, respectively, in each mesh interval S k , (k = 1, . .…”
Section: Radau Pseudospectral Methods For Problem Mmentioning
confidence: 99%
“…In even more recent years, a great deal of research has been done on the class of direct collocation pseudospectral methods. 3,12,16,[18][19][20][21] In a pseudospectral method, the state is approximated using a basis of either Lagrange of Chebyshev polynomials and the dynamics are collocated at points associated with a Gaussian quadrature. The most common collocation points, which are the roots of a linear combination of Legendre polynomials or derivatives of Legendre polynomials, are Legendre-Gauss (LG), Legendre-Gauss-Radau (LGR), and Legendre-Gauss-Lobatto (LGL) points.…”
Section: Introductionmentioning
confidence: 99%
See 1 more Smart Citation
“…, N ) in Eqs. (3) and (5). The total number of LGR points, N = N k K, is obtained by dividing the problem into K mesh intervals using N k LGR points in each mesh interval (for details see Ref.…”
Section: Examplementioning
confidence: 99%
“…The optimal aeroassisted orbital transfer problem is posed as a nonlinear multiple-phase optimal control problem, and the optimal control problem is solved via direct collocation using the Radau collocation hp-adaptive 24 version of the open-source optimal control software GPOPS. [25][26][27] The overall performance of the vehicle is analyzed as a function of the number of atmospheric passes, required inclination change, and maximum allowable heating rate. The results obtained in this study are also compared against a finitethrust all-propulsive orbital transfer.…”
mentioning
confidence: 99%