Longitudinal control stability augmentation control law for amphibious aircraft
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- R&D INST OF CHINA AVIATION IND GENERAL AIRCRAFT
- Publication Date
- 2017-06-13
- Estimated Expiration
- Not applicable · inactive patent
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Figure 1
Abstract
Description
[0001] The technical field mentioned:
[0002] The invention patent relates to the field of aircraft longitudinal control enhancement and stability enhancement control
[0003] Background technique:
[0004] The large-scale amphibious aircraft in service in China adopts a mechanical manpower control system, and the control force is too large, which greatly increases the pilot's control burden and adversely affects the flight quality and flight safety of the aircraft. Although the large-scale amphibious aircraft under development uses a mechanically assisted flight control system, due to the non-return system, the pilot's control burden is still too heavy when the aircraft is in the take-off and landing state, and it is easy to cause large instantaneous changes in attitude when putting out fire and throwing water . In addition, the sea-adaptive and anti-wave capability of this type of aircraft still cannot meet the requirements of open-sea rescue in harsh sea conditions. In ord...