Model-based design uses COTS tools for unmanned aerial systems development
context. This then results in unnecessary rework of the design at a later stage when the power requirement is verified. To address this issue, systems engineers must perform design tradeoffs at the system level and then assess the effect that changes in one subsystem may have on performance of other subsystems and also the overall system performance. To provide meaningful results, design tradeoff studies require system-level models that capture subsystem level dependencies. For example, a typical system-level requirement for an imaging payload is to maintain a certain level of quality for the video transmission throughout flight. One design alternative to evaluate is a high gain, sophisticated control algorithm that enables the UAS to track the target within a few millimeters of accuracy coupled with a low power antenna. At the other extreme is a design with a high power antenna and a less accurate target tracking algorithm. Other design options include varying the video encoding schemes to meet the transmission quality objective. Since these alternatives are not independent, the traditional method of performing design tradeoffs using static analysis in a spreadsheet may lead to a suboptimal design -- or worse, it may lead to the conclusion that the requirements are not achievable. With model-based design, engineers build an executable multi-domain system-level model by connecting GNC and communications models with other interdependent subsystem models. Then, using a variety of subsystem level model components and running parameter sweep simulations, engineers can evaluate the output video image quality to see which design alternatives best meet the system-level performance requirement.Typically when GNC subsystem engineers develop a control algorithm, they use a mathematical model of the plant linked to a model of the control law to analyze closed-loop performance. Traditionally, plant models were developed from measured data or from first principle equations that first had to be solved in closed form so