Allocation of Two Types of Aircraft in Tactical Air War: A Game-Theoretic Analysis
Explicit Guidance Law for Minimum Fuel Horizontal Translation with Bounded Control
Contensou-Busemann conditions for optimal coplanar orbit transfer.
A modified quasi-linearization method for solving trajectory optimization problems.
Quasilinearization determination of optimum finite-thrust orbital transfers.
Mariner MARS Power System Optimization Study Interim Report, 4 Mar. - 31 May 1968
Minimum Sensitivity Design of Attitude Control Systems Final Report
An Optimization Study of the Utias Implosion-Driven Hypervelocity Launcher MK 2
Contractor Support of Fixed and Rotary Wing Aircraft Weapon Systems