Title :
Development and deployment of a performance model for the prototype planetary exploration hopper
Author :
Middleton, Akil ; Paschall, Stephen, II
Author_Institution :
Charles Stark Draper Lab., Inc., Cambridge, MA, USA
Abstract :
This paper describes the development of a detailed model of the TALARIS hopper and demonstrates its performance. TALARIS (Terrestrial Artificial Lunar And Reduced gravIty Simulator) is a small prototype hopping vehicle currently being developed in collaboration between the Massachusetts Institute of Technology and Draper Laboratory. It will serve as an Earth-based testbed for guidance, navigation, and control (GNC) algorithms that will be used to explore lunar and other planetary surfaces remotely. As part of the overall design process, a three degree-of-freedom (3-DOF) performance model called HopperSim was created to simulate the vehicle and run various experiments. First, the design and details of the model are described. Then its capabilities are demonstrated in a study comparing the performance of the Earth-based TALARIS to its Moon-based equivalent. Through HopperSim it is shown that, in 3-DOF, TALARIS can closely emulate a lunar hopper with respect to relevant fight parameters. The model is seen to be a useful tool that can be matured to better predict important details of the performance characteristics of the TALARIS hopper and similar proposed vehicles.
Keywords :
astronomical instruments; lunar surface; space vehicles; 3-degree-of-freedom performance model; Draper Laboratory; Earth-based TALARIS; Earth-based testbed; GNC algorithms; HopperSim; Massachusetts Institute of Technology; TALARIS hopper; Terrestrial Artificial Lunar And Reduced gravity Simulator; fight parameters; hopping vehicle; lunar hopper; lunar surface; planetary surface; prototype planetary exploration hopper; Earth; Fuels; Gravity; Mathematical model; Moon; Trajectory; Vehicles;
Conference_Titel :
Aerospace Conference, 2011 IEEE
Conference_Location :
Big Sky, MT
Print_ISBN :
978-1-4244-7350-2
DOI :
10.1109/AERO.2011.5747509