A solid surface that is in contact with a plasma collects electric charges of impinging electrons and ions. In general, due to the higher differential influx of electrons than that of ions, the surface gets charged negatively, that is, acquires a negative potential with respect to the environment (Whipple, 1981). This potential field exerts a repulsive force for approaching electrons and restrains further inflow of thermal electrons. The equilibrium (or floating) potential is eventually reached when the positive and negative charge inflows are balanced; that is, the net current flow into the surface becomes zero. This concept of current balance holds also in the presence of additional current components that are caused by emission processes of charged particles. The charging process (e.g., Garrett, 1981) and its feedback to plasma environment, such as the formation of sheaths and presheaths (e.g., Robertson, 2013;Scheiner et al., 2015), have been investigated extensively. In space applications, the understanding of charging processes has been developed through long-standing studies of spacecraft charging as well as probe measurements (e.g., Fahleson, 1967;Garrett & Whittlesey, 2000).The surface charging is a significant research area also for the physics of airless, solid planetary bodies in the solar system, such as the Moon and asteroids (Manka, 1973;Stubbs et al., 2014;Zimmerman et al., 2014). This is because charging possibly leads to electrostatic transport of charged dust grains on their surfaces (Nitter et al., 1998;. Such natural bodies covered with nonconducting regolith layers exhibit manifested differential charging depending on both space-environmental and surface conditions. On-orbit observations and theoretical predictions have shown that the darkside and terminator