... three frames. The moments of inertia of the tri‐axis simulator are: Equation 21   Equation 22   Equation 23 where J _i is moment of inertia matrix for body B_i. Spacecraft Simulation Aerodynamics Control technology Artificial satellites...

... regulator are both used at the same time to suppress the vibrations. © Emerald Group Publishing Limited 2009 Systems analysis Piezoelectricity Vibration Control technology Composite materials Plates and shells are the most widely used elements in aeronautics industry and the use...

...‐performance controllers for cruise missiles. Originality/value This is the first paper that adopts an existing single‐range H_∞ controller design procedure to design high‐performance controllers for cruise missiles. © Emerald Group Publishing Limited 2009 Control technology...

... with the MRP as the attitude representation constitutes the value of this paper. In addition, the results obtained in the derivations may be used in future research. © Emerald Group Publishing Limited 2009 Kinematics Control technology Space technology Artificial satellites Linearization...

... for solid propellant launch and ascent vehicles. © Emerald Group Publishing Limited 2009 Trajectories Neural nets Control technology Aerospace engineering T=thrust m=mass q=pitch rate g=gravitational acceleration...

... in Figure 5 when a failure occurs in “Sensor 4” at 7 s. In Figure 6 , the squared residual output can be shown when a fault occurs in “Sensor 4” at 7 s. © Emerald Group Publishing Limited 2008 Control technology Sensors Aircraft Failure (mechanical) Input‐output analysis...

... associated with the developed design procedure: © Emerald Group Publishing Limited 2006 Aerospace transport Control systems Control technology The class of all compensators that stabilize a linear plant G(s) may be parameterized in terms of a function parameter r(s...

... and extends the idea of supervisory controller design to cases when a special state is to be supervised while considering the effect of external disturbances. © Emerald Group Publishing Limited 2006 Aircraft navigation Aircraft components Tracking Control technology a_m...

... navigation Control technology In the past decades, there have not been many attempts to use differential geometric (DG) formulations for the missile guidance problems. Adler (1956) extended the planar PN guidance law to three dimensions, and the three‐dimensional (3D) pure proportional navigation...

... to an appropriate cockpit display. Details available from Trigg Avionics, Tel: +44 (0)131 4498810, E-mail: Andy.davis@trig-avionics.com Aircraft navigation Control technology General aviation transponder Keywords: Aircraft navigation, Control technology The general aviation...