46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference &Amp;amp; Exhibit 2010
DOI: 10.2514/6.2010-7092
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Energy Management of an Aircraft Electrical System

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Cited by 11 publications
(5 citation statements)
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“…For the optimization, P E (t), P I (t), and P A (t) are considered as the optimization variables while T s , P E , P E , SOC E , SOC E , CAP E , P I , and P I are known parameter values provided offline, and δ E (t) and δ I (t) are the online measurements made available from ESRS and PLB1 SDU, respectively, at each time instant t. The CSS OP, as shown in (10) and (11), is a mixed-integer linear programming (MILP) and can be solved using state-of-the-art MILP solvers. The OP is solved at each time instant t based on the system measurements and the known system parameters.…”
Section: Css Optimization Formulationmentioning
confidence: 99%
See 3 more Smart Citations
“…For the optimization, P E (t), P I (t), and P A (t) are considered as the optimization variables while T s , P E , P E , SOC E , SOC E , CAP E , P I , and P I are known parameter values provided offline, and δ E (t) and δ I (t) are the online measurements made available from ESRS and PLB1 SDU, respectively, at each time instant t. The CSS OP, as shown in (10) and (11), is a mixed-integer linear programming (MILP) and can be solved using state-of-the-art MILP solvers. The OP is solved at each time instant t based on the system measurements and the known system parameters.…”
Section: Css Optimization Formulationmentioning
confidence: 99%
“…Assumption 2 provides information about the set point of for the SGN, which is P A (t) = 0. When the PLB1 SDU is activated, the objective function (10) and constraint (6) are considered along with the aforementioned parameter settings for P E (t) and P A (t). Equation (10), when solved for P I (t) and then substituted in (6), produces the following inequality: max P I , δ g1 (t) • P g1 (t) + δ g2 • P g2 (t) − P THy − P E (t) • δ I (t) ≤ P I (t)…”
Section: Plb1 Sdu Rule-based Logicmentioning
confidence: 99%
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“…e electrical equipment operation of the more electric aircraft involves the transmission, interaction, and conversion of the multiphysical domain, such as electrical energy, mechanical energy, hydraulic energy, thermal energy, and information [7,8]. Since the conversion process is dynamic, it is obviously inaccurate to discuss the energy utilization performance simply by using device efficiency, and a digital simulation method is needed [9,10].…”
Section: Introductionmentioning
confidence: 99%