شماره 3 تاریخ انتشار 2627-10-23

• A Modified Midcourse Guidance Law Based on Genelarized Collision Course
• In-Trim Flight Investigations of a Conceptual Fluidic Thrust-Vectored Unmanned Tail-Sitter Aircraft
• COMPARISON BETWEEN MINIMUM AND NEAR MINIMUM TIME OPTIMAL CONTROL OF A FLEXIBLE SLEWING SPACECRAFT
• Robust Integral Sliding-Mode Control of an Aerospace Launch Vehicle
• NORMAL FORM SOLUTION OF REDUCED ORDER OSCILLATING SYSTEMS
• Laminar and Turbulent Aeroheating Predictions around Multi -Cone Configurations in Hypersonic Equilibrium - Air Flow