Add to ORKGAn analytic investigation has been made of procedures for effecting recovery from equilibrium spin conditions for three assumed aircraft configurations. Three approaches which utilize conventional aerodynamic controls are investigated. Included are a constant control recovery mode, optimal recoveries, and a suboptimal control logic patterned after optimal recovery results. The optimal and suboptimal techniques are shown to yield a significant improvement in recovery performance over that attained by using a constant control recovery procedure
An investigation has been made in the Langley 20-foot free-spinning tunnel to determine the erect an...
A preliminarycalculationof an airplanespin-recoverymotionhas been made and the calculationtechniqueh...
The effects of tail design on spin and recovery were investigated in a spin tunnel. A 1/11-scale mod...
The present paper addresses the problem of spin recovery of an aircraft as a nonlinear inverse dynam...
peer reviewedIn this paper, the problem of aircraft spin recovery is solved as a trajectory optimiza...
The present paper addresses the problem of spin recovery of an aircraft as a nonlinear inverse dynam...
Systematic flight investigation of the spinning characteristics of various airplanes over a period o...
An analytical study has been made to investigate the relationship between the magnitude of the appli...
The aim of this thesis research is to extend the previous work of Tapolcai utilizing nonlinearity in...
Incipient- and developed-spin and recovery characteristics of a modern high-speed fighter design wit...
The airplane has a relatively steep spin mode (low angle of attack) with a high load factor and high...
The present paper presents the results of a brief investigation made to determine the effectiveness ...
Incipient- and developed-spin and recovery characteristics of a modern high-speed fighter design wit...
The nonlinear equations of motion are solved algebraically for conditions for which an airplane is i...
A discussion is presented of the type of control manipulation and various techniques that may be req...
An investigation has been made in the Langley 20-foot free-spinning tunnel to determine the erect an...
A preliminarycalculationof an airplanespin-recoverymotionhas been made and the calculationtechniqueh...
The effects of tail design on spin and recovery were investigated in a spin tunnel. A 1/11-scale mod...
The present paper addresses the problem of spin recovery of an aircraft as a nonlinear inverse dynam...
peer reviewedIn this paper, the problem of aircraft spin recovery is solved as a trajectory optimiza...
The present paper addresses the problem of spin recovery of an aircraft as a nonlinear inverse dynam...
Systematic flight investigation of the spinning characteristics of various airplanes over a period o...
An analytical study has been made to investigate the relationship between the magnitude of the appli...
The aim of this thesis research is to extend the previous work of Tapolcai utilizing nonlinearity in...
Incipient- and developed-spin and recovery characteristics of a modern high-speed fighter design wit...
The airplane has a relatively steep spin mode (low angle of attack) with a high load factor and high...
The present paper presents the results of a brief investigation made to determine the effectiveness ...
Incipient- and developed-spin and recovery characteristics of a modern high-speed fighter design wit...
The nonlinear equations of motion are solved algebraically for conditions for which an airplane is i...
A discussion is presented of the type of control manipulation and various techniques that may be req...
An investigation has been made in the Langley 20-foot free-spinning tunnel to determine the erect an...
A preliminarycalculationof an airplanespin-recoverymotionhas been made and the calculationtechniqueh...
The effects of tail design on spin and recovery were investigated in a spin tunnel. A 1/11-scale mod...