Its main technical requirements included: 300 to 400 knots cruising speed, more than 75% hover efficiency, more than 10 cruising lift resistance, useful load of more than 40% of the projected gross weight, bearing -0.5g to 2.0g overload, 4500–5400 kg maximum take-off weight, a ceiling ...
Payload Weight of occupants, fuel and baggage. Useful Load Difference between takeoff weight, and empty weight. Maximum Takeoff Weight Maximum approved weight. 3 Apr 95 1-8 SECTION 2 LIMITATIONS TABLE OF CONTENTS Page General . . . . . . . . . . . . . . . . . . . . . . . ....
station_load.0 to station_load.n Specifies the weight and position of passengers or payload at a station specified with a unique number, station_load.N. The first parameter number on each line specifies the weight (in pounds), followed by the offset relative to datum reference point. The ad...
An adaptive strategy of minimizing energy consumption with lower computational load, has been performed for the lower level, considering the state of charge of the battery and the efficiency of the motor. A sensitivity analysis is performed in a HEPS for a defined aircraft in series architecture,...
When interference over thermal value in a given cell exceeds the threshold value, interference overload indication is transmitted over the backhaul link to all neighboring cells. When a cell receives overload indicator bit set to high, the eNB that controls uplink power, generates closed loop ...
In this study, all analyses regarding the performance of commercial aircraft are directed towards the payload rather than the number of passengers or passenger kilometers for a commercial airliner. In the strict cases where only passengers are transported without any additional cargo load, the weight...
2.2.5 Useful Load Toolbar The Useful Load toolbar (Figure 2.31) consists of four buttons at the bottom of the main window. The Useful Load toolbar buttons can be used to define the aircraft useful load for the current project. The functionality of the buttons on the Useful Load toolbar ...
摘要:A minimum transmission power loss calculation method is proposed, and the specific load configuration is obtained to improve energy transmission capability of the aircraft electric power system. The method is divided into three steps. First, a node table-style format of the aircraft electric pow...
and providing useful information to the operator (such as the presence of dangers to personnel in the vicinity of the UAV). The control system123is configured to adjust the signal of this directional sensor (and any other onboard directional sensors) based on the primary direction of thrust. ...
This requires an exhaustive assessment to be carried out at the flight planning stage, to test all possible combinations of route, payload, fuel load and operating approach, involving tens to hundreds of thousands of calculations per flight. The most optimal scenarios are then ranked in order of...