Hybrid strategy for traffic light detection by combining classical and self‐learning detectors
Hybrid strategy for traffic light detection by combining classical and self-learning detectors
CYCLOIDAL GAIT WITH DOUBLE SUPPORT PHASE FOR THE NAO HUMANOID ROBOT
CYCLOIDAL GAIT WITH DOUBLE SUPPORT PHASE FOR THE NAO HUMANOID ROBOT
Concept of Operations for RCO SPO
Space Radiation Effects on Inflatable Habitat Materials Project
21st Century Space Launch Complex
All FAC(A)s Are Not Created Equal
Aviation Consolidated Allowance List Inspection Process Shortfalls
Automation Architecture for Single Operator, Multiple UAV Command and Control
Single-Seat FAC(A): The Future of the Marine Corps
Use of the Collaborative Optimization Architecture for Launch Vehicle Design
Automating Structural Analysis of Spacecraft Vehicles
Advanced Propulsion Systems for Low-Cost Access to Space
Air-Breathing Launch Vehicle Technology Being Developed
Structural Sizing of a 25,000-lb Payload, Air-Breathing Launch Vehicle For Single-Stage-To-Orbit
Multidisciplinary Performance Analysis of a Lifting-Body Single-Stage-to-Orbit Vehicle
NASA Glenn Research Center's Hypersonic Propulsion Program
Dispersion: A Concept of Employment for Naval Aviation in Operational Maneuver from the Sea
Compact Environmental Anomaly Sensor (CEASE) Flight Integration Support Contract
Control System for the X-33 Linear Aerospike Engine
Assessment of Lifting Body Linear Aerospike Plume Effects on Vehicle Aerodynamics
Near-Optimal Operation of Dual-Fuel Launch Vehicles
Reusable Launch Vehicle Technology Program
Reusable Launch Vehicle Development Research
Advanced Transportation System Studies Technical Area 2(TA-2): Heavy Lift Launch Vehicle Development
Single-Stage-to-Orbit: Meeting the Challenge
Collection of Technical Papers
Abort Performance for a Winged-Body Single-Stage to Orbit Vehicle
Reusable Launch Vehicle: Technology Development and Test Program
Guidance and Control Assessment of Three Vertical Landing Options for RLV
Reusable Launch Vehicle Technology Program and the X-33 Advanced Technology Demonstrator
Transonic Aerodynamic Characteristics of a Proposed Wing-Body Reusable Launch Vehicle Concept
Configurable Technology Development for Reusable Control and Monitor Ground Systems
Launch System Design for Access to Space
Requirements Report for SSTO Vertical Take-off/Horizontal Landing Vehicle
Requirements Report for SSTO Vertical Take-off and Horizontal Landing Vehicle
Single Manager for Air in Vietnam