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
Active wing load alleviation to extend the wing span by 5.8 percent, giving a 3 percent reduction in...
Three designs for controlling loads while rolling for the Active Flexible Wing (AFW) are discussed. ...
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...
The problem of control command and maneuver induced structural loads is an important aspect of any c...
Advances in sensors and avionics computation power suggest real-time structural load measurements co...
This paper describes the maturation of a control allocation technique designed to assist pilots in r...
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...
This paper describes the maturation of a control allocation technique designed to assist pilots in t...
Air travel has had an increasing contribution to global CO2 and non-CO2 emissions, and climate chang...
This paper presents an unusual feedforward controller structure that allows to take allocation const...
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...
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...
Three designs for controlling loads while rolling for the Active Flexible Wing (AFW) are discussed. ...
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...
The problem of control command and maneuver induced structural loads is an important aspect of any c...
Advances in sensors and avionics computation power suggest real-time structural load measurements co...
This paper describes the maturation of a control allocation technique designed to assist pilots in r...
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...
This paper describes the maturation of a control allocation technique designed to assist pilots in t...
Air travel has had an increasing contribution to global CO2 and non-CO2 emissions, and climate chang...
This paper presents an unusual feedforward controller structure that allows to take allocation const...
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...
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...
Three designs for controlling loads while rolling for the Active Flexible Wing (AFW) are discussed. ...
Reduction of aircraft loads, arising as a result of manoeuvre commands or atmospheric turbulence, by...