Development of a Lander Autonomy Testbed for Ocean Worlds Missions/ Exploration and Utilization of Extra-Terrestial Bodies
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Engineering topics
Publications and source records attributed to Jain, A..
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As part of the Space Exploration Analysis and Simulation (SEAS) task, the National Aeronautics and Space Administration (NASA) is using physics-based simulations at NASA's Jet Propulsion Laboratory (JPL) to explore potential surface and near-surface mission operations at Near Earth Objects (NEOs). The simulator is under development at JPL and can be used to provide detailed analysis of various surface and near-surface NEO robotic and human exploration concepts. In this paper we describe the SEAS simulator and provide examples of recent mission systems and operations concepts investigated using the simulation. We also present related analysis work and tools developed for both the SEAS task as well as general modeling, analysis and simulation capabilites for asteroid/small-body objects.
The Lunar Surface Operations Simulator (LSOS) is being developed to support planning and design of space missions to return astronauts to the moon. Vehicles, habitats, dynamic and physical processes and related environment systems are modeled and simulated in LSOS to assist in the visualization and design optimization of systems for lunar surface operations. A parametric analysis tool and a data browser were also implemented to provide an intuitive interface to run multiple simulations and review their results. The simulator and parametric analysis capability are described in this paper.
This paper describes recent developments in the ROAMS physics-based simulator for planetary surface exploration rover vehicles. ROAMS includes models for various subsystems and components of the robotic vehicle including its mechanical subsystem, sensors, on-board resources, on-board control software, the terrain environment and terrain/vehicle interactions. The ROAMS simulator can be used for stand-alone simulation, closed-loop simulations with on-board software or for operator-in-the-loop simulations.
This paper describes the ongoing development of the ROAMS physics-based simulator for planetary surface exploration rover vehicles.
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This paper discusses an approach for sensitivity analysis of multibody dynamics using spatial operators.
This paper tells the story of spatial operators in robot dynamics, emphasizing their physical interpretation, while avoiding lengthly matematical derivations.
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Illustrate use of spatial operators as mathematical tools to make the inherently complex multibody dynamics tractable.
The paper presents a rover execution architecture for controlling multiple, cooperating rovers. The overall goal of this architecture is to coordinate multiple rovers in performing complex tasks for planetary science.
In this paper, we present the development of ROAMS software for real-time simulation of mobile robotic vehicles.
DARTS Shell (Dshell) is a multi-mission spacecraft simulator for development, test, and verification of flight software and hardware.
A MS-Windows based electronic procedure system, called OPIS (Operational Procedure Information System), was developed. The system consists of two parts, the editor, for 'writing' the procedure and the notepad application, for the usage of the procedures by the crew during training and flight. The system is based on standardized, structured procedure format and language. It allows the embedding of sketches, photos, animated graphics and video sequences and the access to off-nominal procedures by linkage to an appropriate database. The system facilitates the work with procedures of different degrees of detail, depending on the training status of the crew. The development of a 'language module' for the automatic translation of the procedures, for example into Russian, is planned.
This paper develops methods for noninteracting control of articulated, possibly flexible, multibody space vehicles based on the diagonalized equation of motion.
A diagonal equation for robot dynamics is developed by combining recent mass matrix factorization results with classical Lagrangian mechanics.
Free-flying space manipulators have a symmetry not normally encountered in terrestrial manipulators, arising from the freedom of choice for the manipulator base-body.
two new methods developed for molecular dynamics simulations of very large proteins are applied to a series of proteins ranging up to the protein capsid of tomato bushy stunt virus.