... A first controller satisfying the handling qualities at stake is provided for a given flight condition, and the goal is to extend its performance to the rest of the flight envelope by sched[r] ...
... The guardian map approach was introduced by Saydy and ...tool for the study of generalized stability of parameterized families of matrices or ...formulation, with respect to a suitable domain Ω in ...
... full control architecture based on MFC techniques, applied to MAV with transitioning flight ...Numerical flight simulations were per- formed in order to validate the interactions between each ...
... priori with a sufficiently high order to realise the desired ...freedom for the resolution of the equality constraints so that the problem is solved by minimising a criteria of type J = ‖K(s) – K ref (s) ‖ ...
... controller with feedforward gain lowered the controller order to make it similar to classical structures usually used in ...Finally, for a given flight condition, we obtained a controller ...
... 8 with α < −0.4) • Damping constraint on the rigid mode (Eq. 9 with ζ > ...0.5 for nom case, ζ > 0.15 for lf and hf cases ) After computation, the algorithm delivers the gains of ...
... In order to stay close to the current schedul- ing methodology (mainly to apply in-flight tun- ing techniques), we have here chosen to develop a stability preserving interpolation technique of existing controllers ...
... irrigation scheduling using a mathemati- cal ...activated for the optimal control problem ...domain for which the relative humidity is below or equal to the threshold of maximal crop ...
... convex maps that are monotone ...nonexpansive for the sup-norm. This includes convex monotone maps that are additively homogeneous ...commute with the addition of ...affine ...
... flying with and without a tail membrane. For the bat model with a tail membrane increasing leg angle increased the lift, drag and pitching moment (nose-down) ...moment with increasing leg ...
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... Due the heading change of the leading aircraft between 220 sec and 310 sec, the value of the slant range decreases to about 4.5 NM before starting to increase Finally, when the [r] ...
... aerobatics with fixed-pitch quadrotors, including triple flips with rotational rates exceeding 1600 deg/s [ 20 ...the flight envelope of the vehicle, making maneuvers such as 180 deg flips, ...
... L’archive ouverte pluridisciplinaire HAL, est destinée au dépôt et à la diffusion de documents scientifiques de niveau recherche, publiés ou non, émanant des établissements d’enseignemen[r] ...
... As in the case of nominal stability, the conditions one needs to check in order to verify time-varying robustness/performance are (1) the frozen-time systems are stable[r] ...
... L’archive ouverte pluridisciplinaire HAL, est destinée au dépôt et à la diffusion de documents scientifiques de niveau recherche, publiés ou non, émanant des établissements d’enseignemen[r] ...
... reccorded for different values of the reference ...system with respect to the apparent inertia J a ...error for a constant apparent inertia J a = 1 ...
... The vehicle will need to change its attitude, which is proportional to the error, but if a loss of altitude is sensed, the velocity controller will attenuate the[r] ...
... of flight performance and decision-making ...inclination for pilots can be to find a way to silence the noise, rather than analyzing the meaning of the alert (Peryer, ...(Avianca Flight 011, Boeing ...
... of scheduling parallel jobs without preemption in multi-processor clusters using the concept of job redirection, where a job can be killed and restarted into a set of dedicated ...processors. Scheduling ...