Add to ORKGThese slide sets describe the OCLA formulation and associated algorithms as a set of new technologies in the first practical application of load limiting flight control utilizing load feedback as a primary control measurement. Slide set one describes Experiment Development and slide set two describes Flight-Test Performance
The implication of the dependence on active controls technology during the design phase of transport...
Active wing load alleviation to extend the wing span by 5.8 percent, giving a 3 percent reduction in...
Reduction of aircraft loads, arising as a result of manoeuvre commands or atmospheric turbulence, by...
These slide sets describe the OCLA formulation and associated algorithms as a set of new technologie...
Advances in sensors and avionics computation power suggest real-time structural load measurements co...
The problem of control command and maneuver induced structural loads is an important aspect of any c...
This paper describes the maturation of a control allocation technique designed to assist pilots in r...
Air travel has had an increasing contribution to global CO2 and non-CO2 emissions, and climate chang...
Feedback laws based upon optimal control theory were derived. and these resulted in a reduction of t...
Air travel has had an increasing contribution to global CO2 and non-CO2 emissions, and climate chang...
Most of the gust load alleviation systems (GLAS) of currently-operational aircraft are of feedback-o...
Most of the gust load alleviation systems (GLAS) of currently-operational aircraft are of feedback-o...
This paper describes the maturation of a control allocation technique designed to assist pilots in t...
Three designs for controlling loads while rolling for the Active Flexible Wing (AFW) are discussed. ...
This paper presents an unusual feedforward controller structure that allows to take allocation const...
The implication of the dependence on active controls technology during the design phase of transport...
Active wing load alleviation to extend the wing span by 5.8 percent, giving a 3 percent reduction in...
Reduction of aircraft loads, arising as a result of manoeuvre commands or atmospheric turbulence, by...
These slide sets describe the OCLA formulation and associated algorithms as a set of new technologie...
Advances in sensors and avionics computation power suggest real-time structural load measurements co...
The problem of control command and maneuver induced structural loads is an important aspect of any c...
This paper describes the maturation of a control allocation technique designed to assist pilots in r...
Air travel has had an increasing contribution to global CO2 and non-CO2 emissions, and climate chang...
Feedback laws based upon optimal control theory were derived. and these resulted in a reduction of t...
Air travel has had an increasing contribution to global CO2 and non-CO2 emissions, and climate chang...
Most of the gust load alleviation systems (GLAS) of currently-operational aircraft are of feedback-o...
Most of the gust load alleviation systems (GLAS) of currently-operational aircraft are of feedback-o...
This paper describes the maturation of a control allocation technique designed to assist pilots in t...
Three designs for controlling loads while rolling for the Active Flexible Wing (AFW) are discussed. ...
This paper presents an unusual feedforward controller structure that allows to take allocation const...
The implication of the dependence on active controls technology during the design phase of transport...
Active wing load alleviation to extend the wing span by 5.8 percent, giving a 3 percent reduction in...
Reduction of aircraft loads, arising as a result of manoeuvre commands or atmospheric turbulence, by...