Abstract:Control systems theory is a wide area covering a range of artificial and physical phenomena. Control systems are systems that are designed to operate under strict specifications, to satisfy certain aims, like safety regulations in the industry, optimal production of goods, disturbance rejection in vehicles, smooth movement and placement of objects in warehousing, regulation of drug administration in medical operations, level control in chemical processes and many more. The present work provides an introduction… Show more
“…Stability requirements specified as gain and phase margins are convenient because they can be measured in a closed loop control system by artificially introducing variations in the loop gain or the phase delay until instability is observed, [1][2][3]. These stability margins can be found analitically by examinating the open-loop tranfer function, Bode diagram, the Nichols Chart gain and the phase cross plot, or the Nyquist plot of real vs. imaginary parts, [6][7][8][9].…”
Section: Quantification Stability Of Aerospace Systemsmentioning
“…Stability requirements specified as gain and phase margins are convenient because they can be measured in a closed loop control system by artificially introducing variations in the loop gain or the phase delay until instability is observed, [1][2][3]. These stability margins can be found analitically by examinating the open-loop tranfer function, Bode diagram, the Nichols Chart gain and the phase cross plot, or the Nyquist plot of real vs. imaginary parts, [6][7][8][9].…”
Section: Quantification Stability Of Aerospace Systemsmentioning
“…ℎ̇= sinθ − cosθsin∅ − cosθcos∅ The rotational kinematic equations, which relate Euler angular rates to body-axis angular rates, are given by ( [4][5][6]…”
Section: )mentioning
confidence: 99%
“…Then, a preprogrammed pitch profile for the flare is commanded. Flying aircraft are controlled by autopilots to follow commanded trajectories, [4][5][6]: The engine used in the B-737 linear Autoland model is Pratt and Whitney JT8D-7. It is an example of the turbofan type of jet engine.…”
Section: Air Traffic Control Operation Systemmentioning
“…The aircraft involved in the conflict are assumed to be flying at constant velocity during a resolution maneuver. [1], [3][4] Now, let's define for aircraft i and aircraft j: [2], [5][6], [7][8][9], [15] …”
Section: Numerical Simulation and Conclusionmentioning
confidence: 99%
“…The key to the JPDA algorithm is the evaluation of the conditional probabilities of the following joint events: [3][4], [5][6], [15] = ⋂ =1 , = 1, … , ; = 0,1, … ,…”
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