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optimization
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keywords:("optimization")
A statistical optimization of the two-impulse transfer maneuver for a fixed-time rendezvous.
Design of optimized three-dimensional thrust nozzle contours
Launch vehicle optimization, phase II. VOLUME I - Concept development and application Final report
Special orbits for the exploration of Mars and Venus
Multi-Objective Hybrid Optimal Control for Interplanetary Mission Planning
Peak-Seeking Optimization of Trim for Reduced Fuel Consumption: Flight-Test Results
Trajectory Optimization of Electric Aircraft Subject to Subsystem Thermal Constraints
A method of approximating propellant requirements of low-thrust trajectories
The flight path control software system of the Lunar Orbiter.
Research achievements in optimization techniques
Game approach to the problem of selecting optimal parameters of a dynamic system
Optimal multistage rocket flight and other discontinuous variational problems
Evaluating the Performance of Hybrid Vehicles between LEO, Cislunar Space, and Mars
Evaluating the Performance of Hybrid Vehicles between LEO, Cislunar Space, and Mars
A general method for determining optimum thrust nozzle contours for gas-particle flows.
Mission logic development and trajectory prediction, determination and optimization Final report
Rapid determination of near-optimum linear pitch programs for rocket boosters.
Optimization problems caused by interaction of guidance and propellant systems.
Optimization problems caused by interaction of guidance and propellant systems.
Simplified Applied Loads of a Transonic Truss-Braced Wing Derived from Computational Fluid Dynamics
Simplified Applied Loads of a Transonic Truss-Braced Wing Derived from Computational Fluid Dynamic
THREE-DIMENSIONAL LOW-THRUST INTERPLANETARY TRAJECTORY OPTIMIZATION
A modified quasi-linearization method for solving trajectory optimization problems.
Optimal payload trajectory characteristics for winged booster vehicles.
Optimum Interplanetary Rendezvous Trajectories With Power-Limited Vehicles
A manual optimal guidance scheme using a predictive model.
Building a pathway to Mars: Mars technology program analysis and case study
Aeroelastic Tailoring Study of N+2 Low Boom Supersonic Commerical Transport Aircraft
Optimization of data return from planetary missions by trajectory design.
Automatic design of optimum Atlas-Agena vehicle trajectories.
Iterative guidance applied to generalized missions.