978 - 1 - 107 - 07094 - 3 - Fundamentals of Aerospace Navigation and Guidance
نویسندگان
چکیده
acceleration, 29, 46–48, 69, 93, 139 of gravity, 93, 152, 161, 264 accelerometers, 109, 114 active constraints, 214 actual flight time approximation ballistic guidance, 165–167 actual state vectors, 2 adherence property (of the supremum), 24, 196 adjoint vectors, 14, 37–39, 46, 137, 142–143, 147, 167–169, 183, 263 equation, 38 state transition matrix, 38 aerospace mission, 6, 289 aileron deflection, 18, 46, 115 altitude, 20, 150, 154, 171, 218 angular momentum, law of, 18 angular velocity, 94–97, 111, 170 vectors, 178, 225, 278 Apollonius Circle Theorum, 273–275 apparent target homing guidance miss, 113–115 displacement, 140 motion, 141 approximate miss distance analysis homing guidance, 124–126 argument at periapse, 227 asteroid, 197–198 asympotically stability, 22–23 asymptotic observer, 96–100, 108 attitude control, 6 autopilot, 7, 130, 132–135, 137, 141, 144, 147, 241, 281
منابع مشابه
07094 - 3 - Fundamentals of Aerospace Navigation and Guidance
The purpose of this book is to present fundamentals used in the navigation and guidance of aerospace vehicles. By fundamentals, we mean a body of knowledge that does not change with advances in technology. Aerospace vehicles encompass all kinds of craft flying in the atmosphere or in space. Navigation is concerned with the questions: Where is the vehicle? What is its velocity? And what are its ...
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