Separate Surfaces for Automatic Flight Controls

The Most Suitable Algorithm for Inverted Pendulum Control

“…The structure consists of the three loops -inner, middle and outer. The form of the inner loop is the same like in previous examples and is given by equation (5 …”

“…4. The model consists also from 2 loops -inner and outer and the transfer function valid for inner loop is given by equation (5 …”

Gemma: A Generic, Extensible and Modular Multi-Sensor Navigation Analysis System

“…Specifically, it is able to achieve the infinitely derivable position and orientation by convolving with a C ∞ function and later on interpolating the resulting trajectory at the rate selected by the user; the realistic orientation for different platforms is obtained from the dynamics formulas of those vehicles (Rajamani, 2011, Roskam, 1995.…”

Static and dynamic analysis of an unconventional plane - Flying wing

“…Under these specifications the minimum requirements for a Class I airplane with flight phase A were that /-=0.19, and & = 1.0 rad/sec. 6 It is known …”

“…Such amplitude and period trends were too slow for a desirable Dutch Roll mode. 6 The Dutch Roll Damping Frequency, was g D =0.068, and the Undamped Dutch Natural Frequency was & = 1.0235 rad/sec. The n D instability predicted by the sign of the real part of the Dutch Roll poles was also corroborated by the necessary criteria for lateral-directional stability which required Q to be negative and with magnitude of half of c • 8 The MATLAB interface predicted that for the n f original configuration, with no winglets, c = -0.0115 h and c =-1.2654 e-4 which did not satisfy the second n t> criteria for lateral-direction stability.…”