NUMERICAL APPROXIMATION OF MULTIVARIATE FUNCTIONS APPLIED TO THE ADAPTIVE GUIDANCE MODE PART II
A method for calculating parachute opening forces for general deployment conditions.
Implementation of an optimal adaptive guidance mode.
A modified quasi-linearization method for solving trajectory optimization problems.
Symmetrical, equilibrium flow past a blunt body at superorbital re-entry speeds.
Predictive Lateral Logic for Numerical Entry Guidance Algorithms
Cowell Type Numerical Integration as Applied to Satellite Orbit Computation
Ill-Conditioning Resulting from Reduced Integration
Attitude Stability of a Class of Partially Flexible Spinning Satellites
Optimal Three Dimensional Reentry Trajectories for APOLLO-Type Vehicles
A Second-Order Artificial Satellite Theory Based on an Intermediate Orbit
Unsteady Aerodynamics and Its Integration in Aeroelastic Analysis
A FIRST ORDER THEORY FOR ROTATING GRAVITY GRADIOMETERS
Deprivation of Newtonian-Type Integration Coefficients and Some Applications to Orbit Calculations