AIAA Scitech 2019 Forum 2019
DOI: 10.2514/6.2019-0646
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Minimum-fuel Powered Descent in the Presence of Random Disturbances

Abstract: It has recently been shown that minimum-fuel powered descent guidance can be solved onboard the spacecraft as a convex optimization problem. It therefore presents itself as a promising technology to enable future planetary exploration missions. However, since this approach is formulated as a deterministic optimal control problem, the resulting guidance law is only designed for a single pair of initial and target states without external disturbances. This paper is an attempt to extend this approach to the more … Show more

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Cited by 21 publications
(19 citation statements)
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“…In future work we plan to apply iCS to problems in entry, descent, and landing (EDL) with nonlinear dynamics, such as entry and powered descent [21]. Another extension to this work would be the addition of time-varying chance constraints that are satisfied for all time, rather than for each time, while not being overly conservative.…”
Section: Discussionmentioning
confidence: 99%
“…In future work we plan to apply iCS to problems in entry, descent, and landing (EDL) with nonlinear dynamics, such as entry and powered descent [21]. Another extension to this work would be the addition of time-varying chance constraints that are satisfied for all time, rather than for each time, while not being overly conservative.…”
Section: Discussionmentioning
confidence: 99%
“…Fortunately, there exist excellent monographs and survey papers on this topic; see [202,203,92,242,5,243,185]. The range of applications has also increased exponentially; we mention quality control, industrial manufacturing, vehicle path planning [205,206], image processing [23], computer graphics [226,227,229,230,231,150], machine learning [228,9,174], and econometrics [109], among others. We shall only briefly review some concepts and results that are relevant to the topics of this paper.…”
Section: Kantorovichmentioning
confidence: 99%
“…This relaxation makes the terminal state less distributed than the target distribution. In many real-world applications [10] it may be preferable to achieve smaller uncertainty in the terminal state.…”
Section: Input-constrained Ocs Problemmentioning
confidence: 99%
“…Such a situation occurs in many real-world scenarios. For example, in aircraft [8] or spacecraft [10] control problems the control command values have physical restrictions such as minimum/maximum thrust.…”
Section: Introductionmentioning
confidence: 99%
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