This paper explores the pursuit-evasion game of two spacecrafts in low coplanar orbit under minute continuous
thrust. By using differential game theory, this study verifies terminal conditions confined by controlling, target set and
velocity and gives the linear game model of minimum error that is compared with nonlinear game model on sight
coordinate. The terminal conditions are fixed by constructing parameter equations set, which are obtained by the optimal
controlling strategy for both spacecraft. Within the linearized set of equations, there are variable parameters that are
associated with the linearization process. Using differential game of kind theory, this paper obtains the expression of the
barrier with the variable parameters to be established. According to extremum theory of the minimum error, the
parameters to be established are achieved. This paper gives the results of theoretical derivation and numerical simulation.
Access to the requested content is limited to institutions that have purchased or subscribe to SPIE eBooks.
You are receiving this notice because your organization may not have SPIE eBooks access.*
*Shibboleth/Open Athens users─please
sign in
to access your institution's subscriptions.
To obtain this item, you may purchase the complete book in print or electronic format on
SPIE.org.
INSTITUTIONAL Select your institution to access the SPIE Digital Library.
PERSONAL Sign in with your SPIE account to access your personal subscriptions or to use specific features such as save to my library, sign up for alerts, save searches, etc.