I. Introduction
Unmanned Aerial Vehicle (UAV) and Unmanned Aircraft Systems (UASs) support technologies have matured to the point where integrated unmanned system ensembles are developed to increase flexibility, operability, range, and endurance. A specific configuration of interest is an integrated ensemble of a Unmanned Ground Vehicle (UGV) as a base vehicle with a landing platform on top, on which multi-rotors and helicopters may takeoff and land and possibly recharge [1], [2]. Modeling and control of such integrated systems is a challenging problem worthy of investigation.