This document describes an algorithm for the generation of a four dimensional trajectory. Input data for this algorithm are similar to an augmented Standard Terminal Arrival (STAR) with the augmentation in the form of altitude or speed crossing restrictions at waypoints on the route. This version of the algorithm accommodates constant radius turns and cruise altitude waypoints with calibrated airspeed, versus Mach, constraints. The algorithm calculates the altitude, speed, along path distance, and along path time for each waypoint. Wind data at each of these waypoints are also used for the calculation of ground speed and turn radius
This document provides a high-level description of several advanced IM operations that NASA is consi...
A critical component of SVS displays is the appropriate presentation of terrain to the pilot. At the...
The objective of this project is to define torque values for bolts and screws when loading is not a ...
This document describes an algorithm for the generation of a four dimensional aircraft trajectory. I...
This paper presents an overview of the seventh revision to an algorithm specifically designed to sup...
This paper presents an overview of the sixth revision to an algorithm specifically designed to suppo...
This paper presents an overview of the fifth revision to an algorithm specifically designed to suppo...
This paper presents an overview of the third major revision to an algorithm specifically designed to...
NASA's NextGen Concepts and Technology Development (CTD) Project focuses on capabilities to improve ...
An investigation of the aeroheating environment of the Project Orion Crew Entry Vehicle has been per...
This document describes the heads-up display (HUD) used in a piloted lifting-body entry, approach an...
The purpose of the Aviation System Analysis Capability (ASAC) Air Cargo Investment Model-Cargo (ACIM...
The Tool for Turbine Engine Closed-Loop Transient Analysis (TTECTrA ver2) is a control design tool t...
The objective of this research by NextGen AeroSciences, LLC is twofold: 1) to deliver an initial "to...
Numerical simulations to assess the effectiveness of Generalized Predictive Control (GPC) for active...
This document provides a high-level description of several advanced IM operations that NASA is consi...
A critical component of SVS displays is the appropriate presentation of terrain to the pilot. At the...
The objective of this project is to define torque values for bolts and screws when loading is not a ...
This document describes an algorithm for the generation of a four dimensional aircraft trajectory. I...
This paper presents an overview of the seventh revision to an algorithm specifically designed to sup...
This paper presents an overview of the sixth revision to an algorithm specifically designed to suppo...
This paper presents an overview of the fifth revision to an algorithm specifically designed to suppo...
This paper presents an overview of the third major revision to an algorithm specifically designed to...
NASA's NextGen Concepts and Technology Development (CTD) Project focuses on capabilities to improve ...
An investigation of the aeroheating environment of the Project Orion Crew Entry Vehicle has been per...
This document describes the heads-up display (HUD) used in a piloted lifting-body entry, approach an...
The purpose of the Aviation System Analysis Capability (ASAC) Air Cargo Investment Model-Cargo (ACIM...
The Tool for Turbine Engine Closed-Loop Transient Analysis (TTECTrA ver2) is a control design tool t...
The objective of this research by NextGen AeroSciences, LLC is twofold: 1) to deliver an initial "to...
Numerical simulations to assess the effectiveness of Generalized Predictive Control (GPC) for active...
This document provides a high-level description of several advanced IM operations that NASA is consi...
A critical component of SVS displays is the appropriate presentation of terrain to the pilot. At the...
The objective of this project is to define torque values for bolts and screws when loading is not a ...