Zobrazeno 1 - 10
of 46
pro vyhledávání: '"Roger H. Hoh"'
Publikováno v:
Journal of the American Helicopter Society. 42:89-95
Publikováno v:
AIAA Atmospheric Flight Mechanics Conference.
Key factors are identified that result in increased potential for rudder overcontrol leading to structural failure of the vertical stabilizer in transport aircraft in up-and-away flight. Rudder sizing and travel are typically defined by requirements
Publikováno v:
Journal of Guidance, Control, and Dynamics. 13:8-15
A fixed base simulation has been performed to investigate the handling qualities requirements for the mid-term pitch response of a helicopter at hover and in low-speed flight. Pilot rating results from this simulation were compared with those from pr
Publikováno v:
AIAA Atmospheric Flight Mechanics Conference and Exhibit.
Autor:
Roger H. Hoh, David G. Mitchell
Publikováno v:
21st Atmospheric Flight Mechanics Conference.
The USAF has undertaken an extensive program to develop a unified method to predict susceptibility to pilot-induced oscillations. This paper describes work done in support of that program. A catalog of PIO time histories has been assembled and key pa
Publikováno v:
Guidance, Navigation, and Control Conference.
A recent effort undertaken for the Air Force Flight Dynamics Directorate provided proposed revisions to the flying qualities military standard. The intent of these revisions was to create the structure necessary for a mission-oriented specification.
Publikováno v:
Guidance, Navigation, and Control Conference.
Publikováno v:
18th Atmospheric Flight Mechanics Conference.
A study aimed at determining the effects of simulator characteristics on perceived handling qualities is discussed. Evaluations were conducted with a baseline set of rotorcraft dynamics, using a simple transfer-function model of an uncoupled helicopt
Autor:
Irving L. Ashkenas, Roger H. Hoh
Publikováno v:
Journal of Aircraft. 14:142-150
A heading control criterion based on the aileron-rudder sequencing required to achieve coordinated turns is presented. Quantification of the aileron-rudder shaping is obtained by consideration of the ideal crossfeed which completely eliminates sidesl