Non-linear Sliding Guidance algorithms for precision lunar landing

Roberto Furfaro, Scott Selnick, Michael L. Cupples, Matthew W. Cribb

Research output: Chapter in Book/Report/Conference proceedingConference contribution

30 Citations (Scopus)

Abstract

Two classes of non-linear guidance algorithms for lunar precision landing are presented. The development of such algorithms is motivated by the need of more stringent landing requirements imposed by future lunar mission architectures (e.g. the ability to land anywhere from a generic lunar orbit). The first class of guidance algorithms, called Optimal Sliding Guidance (OSG) laws, analytically determine the optimal acceleration command and augment it with a sliding mode to provide robustness against perturbations. The second class of guidance algorithms, called Multiple Sliding Surface Guidance (MSSG) laws, employs two interconnected sliding surfaces to track an on-board generated trajectory that drive the descending lander to the desired location at the desired velocity. For both guidance algorithms, which are proven to be globally stable, a set of Monte Carlo simulations have been executed to verify their performances. Both algorithms perform very well, i.e. they exhibit precision a with very low guidance residual errors on the desired target point above the lunar surface. Overall, MSSG shows slightly better performances with two drawbacks: 1) it needs more propellant mass and 2) it requires a higher frequency guidance loop (greater or equal than 100 Hz). The latter it imposes more challenging requirements on the design of the lander avionics system. Conversely, OSG tends to behave in a smoother fashion with excellent landing performance, lower guidance cycle frequency (10 Hz) and less propellant mass. Importantly, MSSG may be employed as real-time guidance scheme to track trajectory generated by more conventional, Apollo-like targeting algorithms.

Original languageEnglish (US)
Title of host publicationAdvances in the Astronautical Sciences
Pages945-964
Number of pages20
Volume140
StatePublished - 2011
Event21st AAS/AIAA Space Flight Mechanics Meeting - New Orleans, LA, United States
Duration: Feb 13 2011Feb 17 2011

Other

Other21st AAS/AIAA Space Flight Mechanics Meeting
CountryUnited States
CityNew Orleans, LA
Period2/13/112/17/11

Fingerprint

Lunar landing
lunar landing
sliding
Landing
Propellants
landing
trajectory
Trajectories
Lunar missions
propellants
Avionics
targeting
Orbits
trajectories
lunar orbits
perturbation
avionics
requirements
lunar surface
commands

ASJC Scopus subject areas

  • Aerospace Engineering
  • Space and Planetary Science

Cite this

Furfaro, R., Selnick, S., Cupples, M. L., & Cribb, M. W. (2011). Non-linear Sliding Guidance algorithms for precision lunar landing. In Advances in the Astronautical Sciences (Vol. 140, pp. 945-964)

Non-linear Sliding Guidance algorithms for precision lunar landing. / Furfaro, Roberto; Selnick, Scott; Cupples, Michael L.; Cribb, Matthew W.

Advances in the Astronautical Sciences. Vol. 140 2011. p. 945-964.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Furfaro, R, Selnick, S, Cupples, ML & Cribb, MW 2011, Non-linear Sliding Guidance algorithms for precision lunar landing. in Advances in the Astronautical Sciences. vol. 140, pp. 945-964, 21st AAS/AIAA Space Flight Mechanics Meeting, New Orleans, LA, United States, 2/13/11.
Furfaro R, Selnick S, Cupples ML, Cribb MW. Non-linear Sliding Guidance algorithms for precision lunar landing. In Advances in the Astronautical Sciences. Vol. 140. 2011. p. 945-964
Furfaro, Roberto ; Selnick, Scott ; Cupples, Michael L. ; Cribb, Matthew W. / Non-linear Sliding Guidance algorithms for precision lunar landing. Advances in the Astronautical Sciences. Vol. 140 2011. pp. 945-964
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