Velocity Requirements for a Soft Landing on Phobos or Deimos in 1969
Use of Planetary Oblateness for Parking-Orbit Alinement
Trajectory Optimization by Explicit Numerical Methods
Trajectories for High Specific Impulse High Specific Power Deep Space Exploration
The Separate Computation of Arcs for Optimal Flight Paths with State Variable Inequality Constraints
Thermal Analysis of the Spacelab Mission D2 Utility Support Structure and Its Payloads
Theoretical Investigation of the Principles and the Design of Equipment for Carrier Energy Dispersal
The Optimization of Multi-Stage Orbit Transfer Processes by Dynamic Programming
Synthesis of the Analytical Results on Optimal Transfers Between Keplerian Orbits
Synthesis of Automatic Flight Control Systems Using Optimal Control Theory
Switch Program Documentation Interim Report, 8 Mar. 1969 - 8 Mar. 1970
Swarm Intelligence for Autonomous UAV Control
Supersonic transport trajectory optimization example solutions Final report