
Accession Number : AD0866450
Title : Report on Navigation.
Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHTPATTERSON AFB OH
Report Date : 29 OCT 1969
Pagination or Media Count : 12
Abstract : The report devises the formula for the linearized range function of a rocket, assuming a known burningcutoff point and velocity at cutoff, a uniform gravitational field and neglecting drag. An estimate of error incurred by the use of this formula is also given. It is shown that only a single accelerometer is needed to evaluate both the position and the velocity vectors.
Descriptors : (*ROCKETS, RANGE(DISTANCE)), GUIDANCE, EQUATIONS, THRUST, ACCELEROMETERS, ROCKET TRAJECTORIES, WEST GERMANY.
Subject Categories : Rockets
Distribution Statement : APPROVED FOR PUBLIC RELEASE