Physics
Scientist
An Approximate Solution of the Euler-Lambert Equation
Controlling the trajectory of a low-thrust spacecraft along the heliocentric portion of the flight from the earth to Mars
Effect of the Composition of the Flight Path Measurements on the Correction of the Flight Path of Space Vehicles
Investigation of Accuracy Requirements of Autonomous Trajectory Measurements to Guarantee Planetary Atmospheric Entry
Optimal One-Parameter Correction of Spacecraft Trajectories
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