Guidance, Navigation and Control
Overview |
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Core Faculty Members |
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Ahmad Bani Younes |
Dr. Bani Younes has been developing a suitable approach to ground-based mobile platform
technology that simultaneously permits large general motions and highly precise inertial
and relative navigation and control, by building the Spacecraft Platform for Astronautics
and Celestial Emulation (SPACE) laboratory. It aims to be a 6DOF facility that supports
comprehensive studies and hardware experiments for sensing, guidance, dynamics, &
control of space operations in an operationally relevant environment. The lab conducts
research in robotic sensing and control with an aim to enhance the fields of proximity
operations, human-robot interaction, stereo vision, swarm robotics, and autonomous
aerial vehicles. This work combines both theory and experiment, including computational
methods in Astrodynamics. Various basic and advanced methods have been explored in
computational celestial mechanics for general N-body problems with arbitrary order
perturbations in order to produce self-tuning, highly parallelizable and efficient
algorithms.
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Jun Chen |
In order to efficiently balance traffic demand and capacity, optimization of Air Traffic
Flow Management (ATFM) relies on accurate predictions of future capacity states. However,
these predictions are inherently uncertain due to factors, such as weather.
This research work presents a novel computationally efficient algorithm to address uncertainty in ATFM by using a chance-constrained optimization method. First, a chance-constrained model is developed based on a previous deterministic Integer Programming optimization model of ATFM to include probabilistic sector capacity constraints. Then, to efficiently solve such a large-scale chance-constrained optimization problem, a polynomial approximation-based approach is applied. The approximation is based on the numerical properties of the Bernstein polynomial, which is capable of effectively controlling the approximation error for both the function value and gradient. Thus, a first-order algorithm is adopted to obtain a satisfactory solution, which is expected to be optimal. Numerical results are reported in order to evaluate the polynomial approximation-based approach by comparing it with the brute-force method. Moreover, since there are massive independent approximation processes in the polynomial approximation-based approach, a distributed computing framework is designed to carry out the computation for this method. This chance-constrained optimization method and its computation platform are potentially helpful in their application to several other domains in air transportation, such as airport surface operations and airline management under uncertainties. ![]()
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Ping Lu
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A hallmark of Prof. Lu’s research program has been addressing real-world challenges in aerospace engineering with academic rigor. In this pursuit Prof. Lu has worked extensively with NASA, DoD, and the Aerospace Industry. Prof. Lu’s research program covers
A current focus is optimal aerocapture guidance and integrated entry and powered landing guidance for pin-point entry and landing of future human Mars missions. ![]()
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