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Flugmechanik
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James Webb Space Telescope Navigation Optimization Challenges
Overview of the Subscale RAVEN Flight Controls and Modeling Testbed
Linear Parameter-Varying Polytopic Modeling and Control Design for Guided Projectiles
Aircraft Certification by Analysis (CbA): 20-year Vision for Virtual Flight Testing
Developing and Sustaining Thermal Protection Systems for Uranus Flagship Mission
Unsteady Aerodynamics in Model-Based Wind Estimation from Fixed-Wing Aircraft Motion
Some Thoughts About the Aerodynamic Pressure Center of Automobile
CFD Analysis of Drag Reduction System (DRS) in Cars
The Aerodynamic Development of Voyah Zhuiguang BEV Version
Feedback Control for Directional Rendezvous Using Constant-Magnitude Low Thrust
Analytical Near-Optimal Distributed Consensus for Cooperative Salvo Guidance
Performance of the Two-Level Targeting Algorithm on Artemis I
Trajectory Design and Early Mission Operations for the Lunar IceCube Mission
Increasing the Dynamic Pressure Capability of the NASA Langley/ODU 6-inch MSBS
Trajectory Design and Early Mission Operations for the Lunar IceCube Mission
Flagship-Class Uranus Orbiter and Probe Using Aerocapture
ACS3 - Flight Dynamics for A Solar Sail Technology Demonstration Mission
Conjunction Assessment Risk Analysis
Challenges of Vehicle Attitude Control Prior to and During On-Orbit Propellant Transfer
Satellite Conjunction Assessment: NASA Best Practices and Lessons Learned
Analysis of a Bank Control Guidance for Aerocapture at Uranus
A Guide to Forced Oscillation Data Processing and Analysis
Artemis I Off-Nominal-Trajectory Design and Optimization
Clustering Approach To Identifying Low Lunar Frozen Orbits In A High-Fidelity Model
Flight Dynamics and Navigation Performance of the BioSentinel Mission
Influence of Electric Propulsion on Performance and Flight Mechanics of VTOL Aircraft
Reducing Landing Site Contamination Using 3-D Trajectory Optimization for Surface Hoppers
Optimized Trajectory Correction Burn Placement for the NASA Artemis II Mission
HLS NRHO to Lunar Surface and Back Mission Design
Development of Aerodynamic Loads Databases for the Space Launch System Booster Separation Event
AeroFusion: Data Fusion and Uncertainty Quantification for Entry Vehicles
Overview of Additively Manufactured TPS Proposed Flight Test and Earth Re-Entry Capsule Design
Wind Tunnel Testing of Static Aerodynamic and Power Consumption Characteristics of an Octocopter
Post-Flight Aerodynamics Assessment of the Artemis-I Booster Separation Event
Aerodynamic Implications of Aerocapture Systems for Uranus Orbiters
Concept Design of a 5 MW Partially Superconducting Generator
Aerodynamics and Performance Flight Research and Airworthiness Best Practices
Application of the CATNLF Design Method to a Transonic Transport Empennage Using CDISC
NASA’s Quiet Electric ENgines (QUEEN): Summary of the QUEEN V2 Test