Abstract
This paper investigates the numerical computation of minimum-fuel low-thrust trajectories subject to bound constraints on the duration of thrust and coast arcs. First, an optimal control problem is formulated. The constraints on thrust and coast periods are written as a single discontinuous bound constraint on the control norm depending on time and on a set of free parameters considered as additional state variables. Then, the constraint is regularized and the problem is converted into an equivalent one where the norm of the control is simply upper-bounded by one. Finally, the latter problem is solved efficiently through an indirect single shooting algorithm. The great advantage of this approach is that it does not require knowing beforehand the control switching profile. Moreover, it has the ability to generate multiple suboptimal solutions in addition to the optimal one, thus offering more options for mission design. Numerical results are provided to illustrate the interest and effectiveness of the method. An electric small satellite rendezvous problem in circular orbit is considered. The fuel-optimal control of the constrained problem as well as several suboptimal controls are computed and analyzed, each of which showing a different number of thrust and coast arcs.
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Disclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.