Possibility of Detection of Exomoons with Inclined Orbits Orbiting Pulsar Planets Using the Time-of-Arrival Analysis

Figure 2

Values of TOA_pert,pm in seconds obtained from (13) for a range of values of the planet mass 𝑀_𝑝 and moon orbit inclination 𝛼. We have also chosen sin𝐼=1, 𝑅=5.2 AU, 𝑟=𝑅/40, and 𝑀_𝑚=𝑀_𝑝/10.