Adjoint Method

Author: Tianjiang Shuo

Website: https://cislunarspace.cn

Definition

A method that constructs the dual system of an original system and uses the dual system's impulse response to compute optimal control inputs. Applicable to time-varying linear systems, transforming multi-impulse maneuver design problems into pseudoinverse solutions.

Application Value

A method that constructs the dual system of an original system and uses the dual system's impulse response to compute optimal control inputs. Applicable to time-varying linear systems, transforming multi-impulse maneuver design problems into pseudoinverse solutions.

  • Bivariate Gaussian Distribution
  • Midcourse Impulse
  • Zero-Thrust Reference Trajectory
  • Co-state Variables

References

  • Bucchioni和Innocenti - 2021 - Rendezvous in Cis-Lunar Space near Rectilinear Halo Orbit Dynamics and Control Issues
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Contributors: ouyangjiahong, Ou Yang Jiahong