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journal of aerospace science and technology
سال:2006 - دوره:3 - شماره:3
A Modified Midcourse Guidance Law Based on Generalized Collision Course
- صفحه:113-123
COMPARISON BETWEEN MINIMUM AND NEAR MINIMUM TIME OPTIMAL CONTROL OF FLEXIBLE SLEWING SPACECRAFT
- صفحه:135-142
In-Trim Flight Investigations of a Conceptual Fluidic Thrust-Vectored Unmanned Tail-Sitter Aircraft
- صفحه:125-133
Laminar and Turbulent Aeroheating Predictions around Multi-Cone Configurations in Hypersonic Equilibrium-Air Flow
- صفحه:159-166
Normal Form Solution of Reduced Order Oscillating Systems
- صفحه:151-158
Robust Integral Sliding-Mode Control of an Aerospace Launch Vehicle
- صفحه:143-149
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