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title: Guidance and Control Conference
μ-Synthesis Control Method for Reentry Vehicle in Large Flight Envelope
Zero Shaping of Nonminimum Phase Aircraft Dynamics (AIAA 2018-0601)
Zero Shaping of Nonminimum Phase Aircraft Dynamics
Zero miss distance of pure PNG
Zero Miss Distance Guidance Using Feedforward and Periodic Control
Zero Miss Distance Guidance Using Feedforward and Periodic Control
Zero-miss-distance guidance law based on line-of-sight rate measurement only
Zero-gyro control of the International Ultraviolet Explorer
Zero Dynamics Analysis for Spacecraft with Fuel Slosh
Zero Dynamics Analysis for Spacecraft with Fuel Slosh
Zernike moment based time sensitive targets detection and recognition
Yaw-Steered Payload Pointing and Orbital Control for a HIEO Spacecraft
Yaw-Steered Payload Pointing and Orbital Control for a HIEO Spacecraft
Yaw Guidance for Airships Under Low Airspeed Conditions
Yaw Guidance for Airships Under Low Airspeed Conditions
Yaw Dynamics Identification of an Insect-Inspired Flapping Wing Micro Air Vehicle (AIAA 2014-1468)
XNAV Program: A New Space Navigation Architecture (AAS 06-007)
XNAV for Deep Space Navigation (AAS 08-054)
XMM-Newton: In-Orbit Performance of the AOCS (AAS 01-076)
XEUS Mission Dynamics Guidance and Control
XACT — A New Generation of Nano GN&C Technology (AAS 15-076)
X-40A Guidance and Control and Flight Test Results (AAS 99-015)
X-38 Vehicle 131R Free Flights 1, 2 & 3: FCS and Aerodynamics Lessions Learned (AAS 02-073)
X-38 Application of Dynamic Inversion Flight Control (AAS 01-016)
X-38 Application of Dynamic Inversion Flight Control
X-34 GNC Trades: A Simple Design for Complex Requirements (AAS 98-025)
X-34 Auto-Landing Guidance, Navigation and Control (AAS 01-013)
X-33 attitude control system design for ascent, transition, and entry flight regimes
X-33 Attitude COntrol System Design for Ascent, Transition, and Entry Flight Regimes
X-33 ascent flight control design by trajectory linearization - A singular perturbation approach
X-31 VECTOR-ESTOL to the Ground Flight Test Results and Lessons Learned
WTA model study of air defense missile system based on particle algorithm
Worst-Case GPS Constellation for Testing Navigation at Geosynchronous Orbit for GOES-R (AAS 13-064)
Worst case dynamic programming and its application to deterministic systems
Worst case analysis of the flight control system X-38 crew return vehicle
Worst Case Analysis of the Flight Control System X-38 Crew Rerum Vehicle
Worst Case Analysis of a Saturated Gust Loads Alleviation System
WorldWide Command and Control: Operating the International Space Station
Working-mode planning of rover in lunar exploration environment
Wireless Wide Area Networked System for Navigation, Communication and Tracking
Wireless vehicle-to-infrastructure data gathering for robot platooning
Wing Flexibility Induced Control Reversal For Flapping Wing Vehicles: Theoretical Analysis
Wing Flexibility Induced Control Reversal For Flapping Wing Vehicles: Observation and Evaluation
Wing Design and Testing for a Tailless Flapping Wing Micro-Air Vehicle
Wingbeat Synchronization And Implementation
Wingbeat Synchronization and Implementation
Wind Uncertainty Correlation and Aircraft Conflict Detection Based on RUC-1 Forecasts AIAA Paper
Wind Uncertainty Correlation and Aircraft Conflict Detection Based on RUC-1 Forecasts
Wind Tunnel Test of an RPV with Shape-Change Effector and Sensor Arrays
Wind Tunnel Test of an RPV with Shape-Change Control Effector and Sensor Arrays