Advances in Aerospace Guidance, Navigation and Control 2017
DOI: 10.1007/978-3-319-65283-2_27
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Attainable Landing Area Computation of a Lunar Lander with Uncertainty by Reachability Analysis

Abstract: Soft landing is one of the most critical phases for space missions which require landing a spacecraft on the surface of a body like asteroids or planets, as well as concepts like reusable launch vehicles. In order to ensure safety and success for the terminal landing phase, in addition to hazard maps obtained by on-board sensors, there is also a need for a map which characterizes the attainable landing area that the lander can achieve by obeying constraints within the presence of uncertainties. This paper prop… Show more

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Cited by 2 publications
(2 citation statements)
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“…In this paper we focus on SPARTAN, an optimal-control package developed by the German Aerospace Center, which has already been used in literature [7][8][9][10][11][12][13] . SPARTAN uses the flipped version of the RPM: the global Flipped Radau Pseudospectral Method (FRPM), based on the flipped distribution of points w.r.t.…”
Section: Pseudospectral Methodsmentioning
confidence: 99%
See 1 more Smart Citation
“…In this paper we focus on SPARTAN, an optimal-control package developed by the German Aerospace Center, which has already been used in literature [7][8][9][10][11][12][13] . SPARTAN uses the flipped version of the RPM: the global Flipped Radau Pseudospectral Method (FRPM), based on the flipped distribution of points w.r.t.…”
Section: Pseudospectral Methodsmentioning
confidence: 99%
“…where (10) and t j are the roots of linear combinations of Legendre Polynomials P n (t) and P n−1 (t). Formal definitions of the Legendre Polynomials can be found in 15 , while an example of Legendre Polynomials of order 0 − 5 is plotted in Fig.…”
Section: A Discretization Of the Ocpmentioning
confidence: 99%