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GPS Pseudolite Signal Design     GPS  Pseudolite  Signal Design       2015/6/29
Pseudolites (PLs), ground-based satellites transmitting GPS-like signals, are becoming increasingly useful for a variety of applications, including differential GPS correction broadcasting and aircraf...
This paper presents an aided dead reckoning navigation system based on the fusion of inexpensive inertial, air data and magnetic sensors aided by a skeletal network of radio-navigation aids. In the fu...
Stanford University has developed a Local Area Augmentation System (LAAS) ground facility prototype known as the Integrity Monitor Testbed (IMT) to demonstrate the feasibility of LAAS precision approa...
This paper demonstrates the tracking and acquisition of GIOVE-A broadcast L1/E5/E6 signals of the Galileo system using a multi-signal all-in-view software receiver. We show that existing aeronautical ...
Young Shin Park is a Ph.D. Candidate in Aeronautics and Astronautics in the Global Positioning System (GPS) Research Laboratory at Stanford University. Her current research interests are enabling LAAS...
This note on Paul Garabedian's work on transonic airfoil and wing design is written from the perspective of aeronautical engineering as well as applied mathematics. Paul's contributions in this area...
A light structure is needed to reduce W0. SFC is the province of the engine manufacturers. The aerodynamic designer should try to maximize VL D . This means the cruising speed V should be increase...
Capability to predict the flow past an airplane in different flight regimes such as take off, cruise, flutter. 2 Interactive design calculations to allow immediate improvement 3 A...
Capability to predict the flow past an airplane in different flight regimes such as take off, cruise, flutter. 2 Interactive design calculations to allow immediate imp...
Aspects of Wing Design     Wing Design  plane       2015/6/18
Another key issue for successful implementation of the continuous adjoint method is the choice of an appropriate inner product for the definition of the gradient. It turns out that there is an...
Aero-Structural Wing Shape and Planform Optimization Fast Time Integration Methods for Unsteady Problems : application to shape optimization of a pitching airfoil • Filtering the Navier Stoke...
Aero dynamic Shap e Optimization fo r Aircraft Design
Advances in technology have begun to make ultra-low Reynolds number flight a real possibility. The growing interest in vehicle development has created a need for an improved understanding of the rele...
A collective is a group of self-motivated agents that maximize system performance through the pursuit of local objectives. This paper deals with two aspects of collective design: the application o...
These notes describe some recent ideas for distributed design and their application to large-scale aerospace systems. In this type of multidisciplinary optimization, design tasks are decomposed in...

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