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Continuing Canadian Leadership in Small-satellite Astronomy
Erratum to: “Space Experiments aboard the Lomonosov MSU Satellite”
Proceedings for the Second Symposium on Space Economy, Space Law and Space Sciences
Proceedings for the Second Symposium on Space Economy, Space Law and Space Sciences
Optical effects produced by running onboard engines of low-earth-orbit spacecraft
In memory of academician Vitaly Lazarevich Ginzburg (October 4, 1916–November 8, 2009)
Erratum to: Space–Time Structures in the Auroral Oval: Approaches to Modeling
Space–Time Structures in the Auroral Oval: Approaches to Modeling
Monitoring the Radiation State of the Near-Earth Space on the Arktika-M No. 1 Satellite
Use of the DBM Model to the Predict of Arrival of Coronal Mass Ejections to the Earth
Postvolcanic Aerosols: Measurements of Altitude and Particle Sizes with Twilight-Sky Polarimetry
Timur Magomedovich Eneev on his 85th birthday
Conceptual Design and Mechanical Analysis of a Lunar Anchored Cislunar Tether
Periodic Approximation of the Rotational Motion of the Photon-12 Satellite
Exploring and interrogating astrophysical data in virtual reality
Stability of a Magnetically Actuated Satellite towards the Sun on a Sun-Synchronous Orbit
Ground Effects and Stability Analysis of Airfoil Accelerated by Electromagnetic Propulsion
Aerodynamic Modeling and Path Optimization of Wing Docking Process for Fixed-Wing UAVs
Wing Design and Adaptive Optimization of a Compound Drone
Stability of resonance rotation of a satellite with respect to its center of mass in the orbit plane
Development and Application Prospect of Space Electric Propulsion Technology
Tandem Observations of Nighttime Mid-Latitude Topside Ionospheric Perturbations
LISA Pathfinder platform stability and drag-free performance
The guiding role of national demand in the first level discipline construction of planetary science
Review, Prospect and Technical Challenge of Launch Vehicle
Birkhoff Pseudospectral Method and Convex Programming for Trajectory Optimization
Simultaneous Trajectory Optimization for Adaptive Powered Descent
Autonomous Descent Guidance via Sequential Pseudospectral Convex Programming
Aerodynamic Parameter Estimation for Launch Vehicles
Ascent Predictive Guidance for Thrust Drop Fault of Launch Vehicles Using Improved GS-MPSP
A Small Peak in the Swarm-LP Plasma Density Data at the Dayside Dip Equator
Autonomous Guidance Control for Ascent Flight
Flutter Regularity of Flying Wing Configuration with All-Moving Wing Tip
A robotic pipeline for fast GRB followup with the Las Cumbrés observatory network