विधियों की तुलना करें

	आनुपातिक मार्गदर्शन	AHRS
क्षेत्र	एयरोस्पेस	एयरोस्पेस
परिवार	Process / pipeline	Process / pipeline
उद्भव वर्ष	1957	1940s
प्रवर्तक	Lin-Hsiung Chu	Aviation heritage
प्रकार	Guidance law	System
मौलिक स्रोत	Knox, W. P. (1971). On optimal proportional navigation. IEEE Transactions on Aerospace and Electronic Systems, AES-7(3), 417–426.	Savage, P. G. (2007). Strapdown Inertial Integration Technology (2nd ed.). Strapdown Associates.
उपनाम	PN, PN law	AHRS system, attitude reference, heading sensor
संबंधित	3	3
सारांश	Proportional Navigation (PN) is a guidance law that generates command accelerations proportional to the rate of change of the line-of-sight angle between a pursuer and target. Introduced by Lin-Hsiung Chu in the 1950s, it became the foundation of modern missile guidance systems. PN solves the pursuit-evasion problem by ensuring that the pursuer intercepts a moving target with minimal computational overhead.	An Attitude Heading Reference System (AHRS) is a complete inertial navigation subsystem that estimates and outputs the three-dimensional orientation (attitude) and heading of a vehicle or platform. AHRS combines measurements from accelerometers, gyroscopes, and often magnetometers through sensor fusion algorithms (typically Kalman filters or complementary filters) to provide a drift-free, fast attitude estimate. AHRS is standard in aviation, marine navigation, and modern autonomous systems.