Zobrazeno 1 - 7
of 7
pro vyhledávání: '"Matthew D. Toniolo"'
Autor:
Peter Finch, Jing Pei, Bandu N. Pamadi, Luke J. Miller, George Z. Bassett, Matthew D. Toniolo, James Grisham
Publikováno v:
2018 Modeling and Simulation Technologies Conference.
This paper describes the development and application of a Generic Control Allocation Toolbox developed at NASA Langley Research Center (LGCAT) intended to aid engineers during the preliminary design phase of an aerospace vehicle. The static controlla
Autor:
Bandu N. Pamadi, Christopher D. Karlgaard, Paul V. Tartabini, Matthew D. Toniolo, Carlos M. Roithmayr
Publikováno v:
Journal of Spacecraft and Rockets. 48:573-583
This paper discusses the application of the constraint force equation methodology and its implementation for multibody separation problems using three specially designed test cases. The first test case involves two rigid bodies connected by a fixed j
Autor:
Christopher D. Karlgaard, Paul V. Tartabini, Robert C. Blanchard, Michael Kirsch, Matthew D. Toniolo
Publikováno v:
Journal of Spacecraft and Rockets. 43:105-115
The formulation and development of a trajectory reconstruction tool for the NASA X-43A/Hyper-X high-speed research vehicle and its implementation for the reconstruction and analysis of flight-test data are discussed. Extended Kalman filtering techniq
Autor:
Christopher D. Karlgaard, Carlos M. Roithmayr, Paul V. Tartabini, Matthew D. Toniolo, Jamshid A. Samareh, Bandu N. Pamadi
Publikováno v:
AIAA Atmospheric Flight Mechanics Conference.
The constraint force equation (CFE) methodology provides a framework for modeling constraint forces and moments acting at joints that connect multiple vehicles. With implementation in Program to Optimize Simulated Trajectories II (POST 2), the CFE pr
Autor:
Bandu N. Pamadi, Matthew D. Toniolo, Carlos M. Roithmayr, Paul V. Tartabini, Christopher D. Karlgaard
Publikováno v:
AIAA Modeling and Simulation Technologies Conference and Exhibit.
This paper discusses the verification of the Constraint Force Equation (CFE) methodology and its implementation in the Program to Optimize Simulated Trajectories II (POST2) for multibody separation problems using three specially designed test cases.
Publikováno v:
46th AIAA Aerospace Sciences Meeting and Exhibit.
This paper discusses a generalized approach to the multi-body separation problems in a launch vehicle staging environment based on constraint force methodology and its implementation into the Program to Optimize Simulated Trajectories II (POST2), a w
Preliminary Dynamic Feasibility and Analysis of a Spherical, Wind-Driven (Tumbleweed), Martian Rover
Autor:
Matthew D. Toniolo, John J. Flick
Publikováno v:
43rd AIAA Aerospace Sciences Meeting and Exhibit.
The process and findings are presented from a preliminary feasibility study examining the dynamics characteristics of a spherical wind-driven (or Tumbleweed) rover, which is intended for exploration of the Martian surface. The results of an initial f