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Flugmechanik
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Analysis of a Bank Control Guidance for Aerocapture at Uranus
In-Space Transportation Sensitivity to Roundtrip Mission Duration and Mars Vicinity Stay Time
Beiträge zur Erhöhung der Flugsicherheit in Windscherungen
On Wings of the Minimum Induced Drag: Spanload Implications for Aircraft and Birds
Long-Term Orbit Operations for the Lunar Reconnaissance Orbiter
A Guide to Forced Oscillation Data Processing and Analysis
OSIRIS-REx Extended Mission Trajectory Design & Target Search
Artemis I Off-Nominal-Trajectory Design and Optimization
James Webb Space Telescope Navigation Optimization Challenges
Active Swarm Resiliency in the HelioSwarm Mission
Active Swarm Resiliency in the HelioSwarm Mission
Navigation Performance Analysis and Trades for the Lunar GNSS Receiver Experiment (LuGRE)
Flexible Aircraft 2 : BMWi-Technologievorhaben ; final report ; composition of publications
Flexible Aircraft 2 : BMWi-Technologievorhaben ; final report ; composition of publications
Recent Improvements to the Copernicus Trajectory Design and Optimization System
Clustering Approach To Identifying Low Lunar Frozen Orbits In A High-Fidelity Model
Flight Dynamics and Navigation Performance of the BioSentinel Mission
Reducing Landing Site Contamination Using 3-D Trajectory Optimization for Surface Hoppers
Attitude Profile Reference for the Earth Orbit Raising Phase of NASA Gateway’s Co-Manifested Vehicle
Trajectory Shaping of Lunar Descent Approach Phase for Human Landing Systems
Mars Reconnaissance Orbiter Operational Aerobraking Phase Assessment
Fallschirmsysteme der DFVLR zur Stabilisierung und Bergung von Flugkörpern
Aerodynamic Coefficients of a 70-deg Spherecone in Hypersonic Flow
HelioSwarm: Swarm Design Methods in Eccentric P/2 Lunar Resonant Orbit
Orbital Drag Near Small Bodies Due to Lofted Fines from Surface Activity
Delta-V Budgets for Robotic and Human Exploration of Phobos and Deimos
HelioSwarm: Relative Orbit Maintenance in Eccentric P/2 Lunar Resonant Orbit
Collision Avoidance “Short Course” Part III: CA in Changing Space Flight Environment
Design loads for future aircraft : = Les charges de calcul pour de futurs aéronefs
HelioSwarm: Relative Orbit Maintenance in Eccentric P/2 Lunar Resonant Orbit
Optimized Trajectory Correction Burn Placement for the NASA Artemis II Mission
Overview of the Subscale RAVEN Flight Controls and Modeling Testbed
HLS NRHO to Lunar Surface and Back Mission Design
Development of Aerodynamic Loads Databases for the Space Launch System Booster Separation Event
Experimental Characterization of the Space Launch System Block 1B Liftoff and Transition Environment
Validierung nichtlinearer Schätzfilter mit erweiterten Modellen für Flugzeug und Meßsystem
DGLR-Fachgruppe 4 "Flugmechanik und Flugfuehrung" Taetigkeit der Fachausschuesse 1972, Koeln